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General Forums => Aircraft and Vehicles => Topic started by: loony1 on February 08, 2007, 10:59:20 AM

Title: Spit 16
Post by: loony1 on February 08, 2007, 10:59:20 AM
something needs to be done about the spit 16 it is totally over modeled

turns inside a zero
speed of a tempest


i find it hard to believe that this is accurate...i don't know how many times i have came across a spit 16 and no mater what i am in he can almost always out turn me or out run me and i know its not just me, so i don't need any flames on my flying skills. I am not the only one who can attest to this. Please check and fix the modeling problem
Title: Spit 16
Post by: AKDogg on February 08, 2007, 11:07:49 AM
I have no problem with spit16

My hog is faster and can turn inside a spit16 all day long
Title: Spit 16
Post by: Simaril on February 08, 2007, 11:42:08 AM
Looney :

No flaming intended.

But the SPit XVI is not the problem. The XVI cannot outrun a tempest GIVEN EQUAL ENERGY AT THE START. Likewise, it cannot outturn a zero at low speed with equal energy.

The Spit XVI is very good at acceleration, very good at climbing. it tunrs well (though not as well as the VIII, or the zero for that matter), and it rolls well.  It will outaccelerate the tempest at low speed, but the tempest wins when accelerating from a faster speed. The Spit XVi on the deck is more than 50mph slower than the tempest, and its turn diameter is AT LEAST 100 feet larger than the zeros at every single flap setting.

Those are the facts.

If you can't beat the thing, then you are probably playing it's game. Don't play to the strengths of your enemy, and you will do much better! I am far from an ace pilot, but spits XVIs don't worry me unless I've made the mistake of giving them the advantage they'd want to begin with.
 

I read your post to say that if you're caught low and slow, you cant so much against them. Yeah, that's proabbly true -- because they will either outpower (like against a zero) or outturn (that tempest -- its not outrunning it, its out ACCELERATING you). Remember that climb and acceleration -- it's honestly the thing I worry about most.

So if you're in spitfire zone, dont let yourself get slow enough that the spit's acceleration would pose a problem.
Title: Re: Spit 16
Post by: Lusche on February 08, 2007, 11:57:02 AM
Quote
Originally posted by loony1
something needs to be done about the spit 16 it is totally over modeled

turns inside a zero
speed of a tempest
 


Speed of a tempest??? Do you actually play this game????

(BTW, wrong forum ;) )
Title: Spit 16
Post by: loony1 on February 08, 2007, 02:22:16 PM
yea doh....sorry bout the wrong forum...ment to be in bug report

anyway here is a scenario for ya..

I'm in a seafire and run into a spit 16 we wind up with a few split Ss then into the turn we go....flaps out.....pulling hard back and he turns inside me and kills me....Happens all the time and has happen in a zero to me also.


next one....i'm in a tempest at 8000ft....i spot a spit 1k above me...he rolls over and starts a dive to get on my 6. I avoid the pass and cause the overshoot and Wep on and  dive hard to the deck...the spit 16 turns hard and dives after me...wooosh...her he comes on my 6 fast as lightning and shoots me down. Now 1. i would sure think he would lose allot of E in the hard turn and 2. I would think the temp should get E up much faster with wep on and almost no E loss and diving hard
Title: Spit 16
Post by: nickf620 on February 08, 2007, 05:45:12 PM
spit 16 has better acceleration also given his speed gained in the dive he was able to get on your 6
Title: Spit 16
Post by: Shamus on February 08, 2007, 08:35:53 PM
Grab a ki84, get him under 200 low, then he's toast:)

shamus
Title: Spit 16
Post by: Oleg on February 09, 2007, 12:36:57 AM
Quote
Originally posted by loony1
I'm in a seafire and run into a spit 16 we wind up with a few split Ss then into the turn we go....flaps out.....pulling hard back and he turns inside me and kills me....Happens all the time and has happen in a zero to me also.


If you cannt outturn Spit16 in Seafire you have BIG problems :rolleyes:
Title: Spit 16
Post by: Simaril on February 09, 2007, 07:23:01 AM
I'd seriously bet that the spit XVI used the vertical to get inside your turn -- a co-e yoyo beats a flat turn every single time.

Film these, and you'll likely see the reason they happen...energy (speed^2 * alt) and tactics probably explain both your scenarios.
Title: Spit 16
Post by: Knegel on February 09, 2007, 08:21:52 AM
Hi,

i have to agree to two strange things happen with the 16.

1. In oposide to all other heavyer wingloaded planes, the 16 with its clipped wings(smaler wingarea) keep more energy than the normal winged Spits.

2. The 16 have a even more smooth stall behaviour than the normal winged Spits.


To 1. this is absolut ok, so there is nothing strange, its rather strange this behaviour dont count for even more heavy wingloaded planes!!  A FW190A8 or a P38(no flaps) bleed energy like mad while the smothest turn.  That the 16 dont bleed energy like mad  simply dont fit into this line!

To 2.

The 16 should lose much of the typical Spit turnperformence at slow speed, but specialy it should tend to be very unstable.

The CW spit had a VERY smal aspectratio, with this and the missing washout effect, it should be much more dangerus(if i remember right thats what the pilots was complaining).

btw, the good slowspeed acceleration of the 16 is related to a horizontal flight and climb, while a dive the relation should shift much toward the planes with a better drag/load.  

And of course a F4U-4 can do all better than the 16, due to its magical flaps.

All over the 16 is far less overmodeled than the F4U´s(due to the magical flaps), the La7 and HurriIIc.

Another btw.  a much more tight turning 16(than a Seafire), can be related to a different fuelload.

I would like to see that the E-bleed get more credible all over.  Heavy wingloaded planes should keep energy like mad while highspeed manouvers and i hate the magical flaps, which particular help to overcome the high e-bleed in some heavy planes.

Greetings,

Knegel
Title: Spit 16
Post by: BaldEagl on February 09, 2007, 09:53:48 AM
The Spit XVI absolutely will not turn inside a Zeke or a Seafire.  If that's consitantly true for you then it sounds like you've got the stall limiter enbled.

I flew a Spit XVI last night alongside a squad mate in a Typhoon.  I was faster climbing and in level flight but in a dive we were'nt even close.  He zoomed away from me like i was standing still.  I'd guess the Temp would be even faster than the Typh.
Title: Spit 16
Post by: Major Biggles on February 09, 2007, 10:02:58 AM
sounds like you were killed by a better opponent loony ;)


as for the spit16 having easy stall behaviour, that's not true, it's very twitchy. it's purely because of the powerful engine and climbrate that it can hang on the prop like it does, which gives the appearance of easy stall handling.

infact, the spit16 is undermodelled, or atleast, it uses a lower power setting than normal. our spit gets 18 pounds of boost at wep, when at the height of it's service it could attain 21 normally, or be pushed to 25 pounds. thank your lucky stars we don't have a 25 lb spit16, the thing climbed at near 6000ft/min and was far faster than our model ;) :lol
Title: Spit 16
Post by: MiloMorai on February 09, 2007, 11:26:30 AM
The Merlin Spits had 18lb boost with 100/130 fuel and 25lb boost with 100/150 fuel.

The RR engine that used 21lb boost was the Griffon.

More like 5000f/m Major.  http://www.spitfireperformance.com/spitfire-IX.html
Title: Spit 16
Post by: Major Biggles on February 09, 2007, 11:42:38 AM
Quote
Originally posted by MiloMorai
The Merlin Spits had 18lb boost with 100/130 fuel and 25lb boost with 100/150 fuel.

The RR engine that used 21lb boost was the Griffon.

More like 5000f/m Major.  http://www.spitfireperformance.com/spitfire-IX.html



ah rgr, thanks milo.

currently our spit does about 4600 ft/min but at 25 boost it was supposed to be 5700 ft/min wasn't it?
Title: Spit 16
Post by: Major Biggles on February 09, 2007, 11:46:57 AM
your site states that a spit9 at 25 boost would achieve 5740 ft/min on a merlin 66. i'd say that's pretty much what the 16 would do, if not slightly better


so roughly 6000ft/min was correct ;)

but thanks for clearing up the boost settings issue :)
Title: Spit 16
Post by: Widewing on February 09, 2007, 12:16:43 PM
Quote
Originally posted by Oleg
If you cannt outturn Spit16 in Seafire you have BIG problems :rolleyes:


Not always true... They have nearly identical turning radii. People forget that the Seafire had its weight corrected and its turn radius suffered for it. Inasmuch as the Mk.XVI offers much better acceleration and power, it can match the Seafire is turning circles without much sweating. Since it can take the fight up hill with ease, the Seafire quickly finds itself in deep bandini.

Equal pilots; the Seafire will lose.

My regards,

Widewing
Title: Spit 16
Post by: Guppy35 on February 09, 2007, 12:21:57 PM
Hmmm,  just last night I got jumped by a Spit XVI while I was in my G.  We went round and round and he was trying to use the vertical as well.  He had more E and alt to begin with.  Somehow or another, if it's the miracle plane some claim it to be, my uber P38G was able to follow him up when he tried that, and was able to get inside his turn to the point I was able to reverse spots with him and killed him.

He must have had a faulty Spit 16? :)

Was a fun fight though.
Title: Spit 16
Post by: MiloMorai on February 09, 2007, 12:23:14 PM
It is also with radiator shutters closed. Open shutters will reduce the roc. Look at the other JL165 report.

Also if you look at the graph, the rate is good to ~500ft.
Title: Spit 16
Post by: Oleg on February 09, 2007, 12:27:43 PM
Quote
Originally posted by Widewing
Equal pilots; the Seafire will lose.


Hmm... How worse Seafire turns in comparison with Spit5?
Title: Spit 16
Post by: Widewing on February 09, 2007, 12:37:32 PM
Quote
Originally posted by Oleg
Hmm... How worse Seafire turns in comparison with Spit5?


Minimum turn radius from my own testing:

Spit Mk.V: 388 feet

Seafire Mk.II: 445 feet

Spit Mk.XVI: 449 feet

Spit Mk.VIII: 442 feet

Spit Mk.IX: 434 feet

My regards,

Widewing
Title: Spit 16
Post by: Knegel on February 09, 2007, 12:57:06 PM
Quote
Originally posted by Major Biggles
sounds like you were killed by a better opponent loony ;)


as for the spit16 having easy stall behaviour, that's not true, it's very twitchy. it's purely because of the powerful engine and climbrate that it can hang on the prop like it does, which gives the appearance of easy stall handling.

infact, the spit16 is undermodelled, or atleast, it uses a lower power setting than normal. our spit gets 18 pounds of boost at wep, when at the height of it's service it could attain 21 normally, or be pushed to 25 pounds. thank your lucky stars we don't have a 25 lb spit16, the thing climbed at near 6000ft/min and was far faster than our model ;) :lol


The stallbehaviour of the Spit16 is very twitchy???

You talk about the real 16,  not the AH one, right??

The 16 in AH behave like a 8 or 9 while a stall, a very nice early stall warning, with the "half stalled" flight, which is supposed to be typical for the full wing Spit, but i doubt it will be the same for the cw Spit.

For me it feels like the 16 got all advantages of the clipped wing, but not the disadvantages.

Greetings,

Knegel
Title: Spit 16
Post by: Knegel on February 09, 2007, 01:01:59 PM
Quote
Originally posted by Guppy35
Hmmm,  just last night I got jumped by a Spit XVI while I was in my G.  We went round and round and he was trying to use the vertical as well.  He had more E and alt to begin with.  Somehow or another, if it's the miracle plane some claim it to be, my uber P38G was able to follow him up when he tried that, and was able to get inside his turn to the point I was able to reverse spots with him and killed him.

He must have had a faulty Spit 16? :)

Was a fun fight though.


Try the same without the "magical flaps". ;)

But maybe he was out of wep and had much fuel, while you had wep and smal fuel.  Fuel and wep change a lot.
Title: Spit 16
Post by: Bronk on February 09, 2007, 01:04:23 PM
Always good to keep at least 1 or 2 luftwhiners around.

Bronk
Title: Spit 16
Post by: Guppy35 on February 09, 2007, 01:09:53 PM
Quote
Originally posted by Knegel
Try the same without the "magical flaps". ;)

But maybe he was out of wep and had much fuel, while you had wep and smal fuel.  Fuel and wep change a lot.


No wep in a 38G :)  Not sure what the magical flaps are.

My point is, that I don't see the 16 as uber.    If it's being flown by a really good stick, they can make it do things I can't.  But the average AH pilot in a 16 doesn't make it do magical things.

I think that applies to any number of birds in here.  There are guys who can do things in P47s I can't even imagine trying.  

I just think that folks are too quick to blame the FM when they get in a situation they normally control and can't.

As for the flight characteristics of the 16.  I find the stall is sharper then the IX or VIII because of the clipped wings.  It tends to drop a wing much quicker with less 'warning'.

I still prefer the VIII to the 16 for that reason among others.  I also believe that the VIII will out turn the 16 because of the regular span wings, and in combats with 16s have not seen differently unless the other guy has turned out to be one of those guys who can do things in a Spit that I can't
Title: Spit 16
Post by: Noir on February 09, 2007, 06:28:02 PM
the 16 will loose against long winged spits in a stall fight, the hard part is to get em to their limit. I recommend using a spit 9 :aok
Title: Spit 16
Post by: Debonair on February 10, 2007, 12:22:08 AM
Spit's wing has washout, unique amongst WWII fighters i think.
Supermarine test pilot Jeffrey Quill wrote that F.16 Spits were the most manuverable of them all...:noid
Title: Spit 16
Post by: BaldEagl on February 10, 2007, 02:30:41 AM
If all the other Spits are so good why can I beat them consistantly with a XVI?  I've had VIII's, IX's and Seafires for lunch in many differing scenarios and many hard fought, fun fights.  Have I been beaten by them?  Yes, of course, but the ratio is by far in the XVI's favor.  

The only Mark that will give the XVI a true contest in my opinion is the V because they share so little among the family.  The V against the XVI becomes a true test of horsepower vs. turning ability, slash and burn against turn and burn.  Against all the others simple throttle control and e management give the XVI an advantage.

And BTW, the stall handling of the XVI, while I agree is somewhat twitchy, is fine once you learn to finess it.  It will hang in a slo-mo pursuit stall as well as any other plane and come back to life more quickly than most if needed.

All of tht said, the K/D stats on the XVI overall are abysmal (1.3 one camp that I checked) so they must not be THAT easy to  fly or else every noob in the game grabs a XVI and dies and a few pilots that fly "dweeb rides" keep the scores up.

Personally, I prefer the V.  I think it's superior to every other Mark and it fits my style like a glove.
Title: Spit 16
Post by: Oleg on February 10, 2007, 02:40:10 AM
I outturn A6M2 in P-40E one or two times, does it means p-40 turns better?

Personally, i count Spit16 as easy kill when i am in corsair-d.

Add:
Just to make it clear, i prefer spit16 over any other spits, it very dangerous plane in right hands and good for newbs (if they dont only HO&run of course). But it neither uber nor overmodelled.
Title: I'm with Oleg
Post by: Patches1 on February 10, 2007, 04:02:44 AM
Spit xvi even easier to kill while flying an F4U-1 Corsair.

No magical flaps, just good SA gets the kill on a 16.

Just my opinion.
Title: Spit 16
Post by: Blagard on February 10, 2007, 06:19:20 AM
Quote
Originally posted by BaldEagl
If all the other Spits are so good why can I beat them consistantly with a XVI?
Have you considered that you might just fly that version better ?
Title: Spit 16
Post by: Widewing on February 10, 2007, 09:35:59 AM
Quote
Originally posted by BaldEagl
If all the other Spits are so good why can I beat them consistantly with a XVI?  I've had VIII's, IX's and Seafires for lunch in many differing scenarios and many hard fought, fun fights.  Have I been beaten by them?  Yes, of course, but the ratio is by far in the XVI's favor.  


You cannot determine the capability of any fighter based upon experiences in the Main Arenas. Most of the players flying in the arenas are cannon fodder in a 1v1 fight. There are only a handful of highly skilled pilots that consistently fly Spitfires in the Main Arenas. Spitfires and P-51s are the fighters most commonly selected by n00bs in the TA. This often carries over to the Main Arenas.

I have my own rating standard for Spitfires, which I categorize by altitude.

Low alt: Sea level to 8,000 ft
SpitVIII - A little bit slower than the XVI, but similar acceleration and climb. Better turn and stability.
SpitXVI - Great E fighter, average turn fighter.
SpitIX - The forgotten Spitfire. Out-turns the VIII and XVI, gets better as you go up.
SpitXIV - Pure E fighter. Needs altitude to shine.
SpitV - Great turn fighter, but dominated by later models in everything but stall-fights.
Seafire - Too heavy for its available power.
SpitI - Eight .303s and gravity fed carburetor undo this model. Very poor roll at speeds over 350 mph.

Medium alt: 8,000 ft to 18,000 ft.
SpitVIII - Still offers excellent performance.
SpitIX - Coming into its element.
SpitXVI - beginning to lose its edge as you approach 15k.
SpitXIV - Good speed, climb and acceleration, but needs more alt to really excel.
SpitV - Not enough speed, climb and acceleration to compete with those above.
Seafire - Same issues as above.
SpitI -  same issues as above.

High Alt: 18,000 ft to 30,000 ft
SpitXIV - Up high, this Spitfire has few peers.
SpitIX - Up here, the Merlin 61 can strut its stuff.
SpitVIII - Out of its element, but still good enough to be a real threat.
SpitXVI - Also out of its element. Clipped wings pay a big penalty up high.
SpitV - At high altitude, speed is king. The MkV doesn't have much speed up high.
Seafire - Far too high for this fighter. Badly outclassed up here.
SpitI -  Same issues as before, but exacerbated.

My regards,

Widewing
Title: Spit 16
Post by: VooWho on February 10, 2007, 11:00:06 AM
I have film of me offline in spit16. I just took it up in the air and did some other things. I don't know how to post it.
Title: Spit 16
Post by: Guppy35 on February 10, 2007, 11:26:24 AM
Quote
Originally posted by BaldEagl
If all the other Spits are so good why can I beat them consistantly with a XVI?  I've had VIII's, IX's and Seafires for lunch in many differing scenarios and many hard fought, fun fights.  Have I been beaten by them?  Yes, of course, but the ratio is by far in the XVI's favor.  

The only Mark that will give the XVI a true contest in my opinion is the V because they share so little among the family.  The V against the XVI becomes a true test of horsepower vs. turning ability, slash and burn against turn and burn.  Against all the others simple throttle control and e management give the XVI an advantage.

And BTW, the stall handling of the XVI, while I agree is somewhat twitchy, is fine once you learn to finess it.  It will hang in a slo-mo pursuit stall as well as any other plane and come back to life more quickly than most if needed.

All of tht said, the K/D stats on the XVI overall are abysmal (1.3 one camp that I checked) so they must not be THAT easy to  fly or else every noob in the game grabs a XVI and dies and a few pilots that fly "dweeb rides" keep the scores up.

Personally, I prefer the V.  I think it's superior to every other Mark and it fits my style like a glove.


You've answered your own questions.  You know how to use the XVI well and that's the difference.

So far this tour I'm 7-1 vs 16s and the death was when he picked me while i was in with 3 other guys.  I've had a bunch of 1 v 1s against 16s in my 38G and I keep winning them.

Does that mean the 38G is uber and the Spit sucks?  Nah.  I've just reached the point where I know what I can do in my 38G just like you know what to do in your 16.  If I can get em to fight my fight, I'm ok.

Do keep in mind however that the Spit 16 could just as easily be called the Spit LFIXe.  I'd like to believe it was at our suggestion that Pyro went with the XVI instead of LFIX just to give us a different model number.    Same bird otherwise.

In retrospect it probably would have been better to name it the LFIXe and let the skinners be able to skin 16s as well on it.  I'm guessing folks would be much less worried about it if the number was 9 instead of 16.
Title: Spit 16
Post by: SuperDud on February 10, 2007, 08:21:19 PM
Nice write up WW!
Title: Spit 16
Post by: Benny Moore on February 10, 2007, 08:41:01 PM
Quote
Originally posted by Knegel
Try the same without the "magical flaps".


They're called Fowler flaps, and why would anyone not want to use them?  Even the Pilots Manual for the Lockheed P-38 Lightning recommended using the Fowler flaps for turning.  A fighter that heavy needs them to be competitive with lighter kites.
Title: Re: Spit 16
Post by: Serenity on February 11, 2007, 01:25:40 AM
Quote
Originally posted by loony1

turns inside a zero


Nope. Spitfire mk IX, VIII, V, Seafire IIc, and Spitfire mk I all turn inside it, not to mention Hurricanes and of course zeros. You were in a bad E-state. I completely agree they are overmodelled, but they are bad turners. The error I beleive, is in its lift and the strenght of the engine. It hovers. Its a UFO. It needs to be fixed.
Title: Spit 16
Post by: Serenity on February 11, 2007, 01:29:09 AM
Oh, and yeah. the Spixteen has issues, again in the vertical. THats where its screwed up. Its VERY easy to kill. It really is. Any turn fighter, and any P-40E can easily incinerate one. Just never challenge it in the vertical. Thats why the kill stats are down. n00bs TnB, and thats where they get eaten. As soon as they learn to climb they are unstoppable.

lol Guppy. Im not so sure. Im more afraid of mk IXs than spixteens, because the only ones who fly the mk IX, are the ones who know how to fight. The same WOULD go for the V, but I know a lot of n00bs who are knowlageable (Yeah, I spelled that wrong, its been a long day) enough to recognize the V, and have been warned not to fly the Spixteen then go to Vs and are again baby seals. There are many more good pilots in mk Vs than in XVIs, I find. Id like to see the XVIe though. The non-clipped. Im curious as to if it too would be a UFO here.
Title: Spit 16
Post by: Knegel on February 12, 2007, 02:29:01 PM
Quote
Originally posted by Benny Moore
They're called Fowler flaps, and why would anyone not want to use them?  Even the Pilots Manual for the Lockheed P-38 Lightning recommended using the Fowler flaps for turning.  A fighter that heavy needs them to be competitive with lighter kites.


I know fowlerflaps, but i never saw fowler flaps that double the liftfactor of a wing without to increase the drag dramatically, but thats what many flaps in AH do and thats why i call them "magic flaps".

Although the fowler flaps was more effective than most other systems, they dont made the P38 to a good sustained turning plane, like it is in AH!!

The P38 was know as a very good B&Z plane and the pilots wrote, "with help of the combat flaps, we could turn inside the smaler planes", to turn inside a plane dont mean to turn with it!!

Imho the AH P38 have a to high E-bleed without using the flaps, what make this "magical flaps" needed to provide a somewhat credible result, while the way to get this result isnt credible.

Same count for the magical F4U flaps, while the F4U without the flaps already show the great realistic advantages of this plane(high speed, good upzoom, good roll), this "magical flaps" in combination with its realistic advantages make the F4U (specialy the -4) to the monster dweeb plane in AH.

btw, this have nothing to do with Luftwhining, the 109F also behave to good in relation to the other 109´s and the A6M5 keep to much energy at highspeed(similar to the HurriIIc).

In hands of a good pilot the 16 was probably one of the best low level dogfighters in WWII, but according to the pilots already the normal winged Spits did need a good pilot cause the very light elevator, the cw Spit did count as even more difficult regarding the usage of the elevator.
Absolut nothing of this i can find in AH. Who wanna know how bad slowspeed handling and difficult stall behaviour feels in AH, should try the Ta152 at slow speed. In Ta152 the aspectratio related high lift dont seems to work, in oposide to the P38. Even with 25% fuel the Ta snap roll extreme from one side to the next at 105mph(engine out, so torque isnt a argument), while the extreme heavy wingloaded(100% fuel) P38L dont snaproll at all and lower the nose at 95mph(no flaps). The Spit16 lower its nose at 70-80mph and if a roll happen, its rather smoth.

Since the Ta152H is one of the few german planes that got rated as very good even by the allied testilots, i will compare it with the P38L and Spit16:

Wingload:
P38L(100% fuel): 260kg/m²
Spit16(100% fuel) : 158kg/m²
Ta152H(25% fuel): 188kg/m²

Wing aspect ratio(one of the best arguments to explain the good P38 behaviour, despite its high wingload and this is a absolut valid argument. The Aspecratio is at least as important as the wingarea, specialy if it comes to slowspeed lift/drag behaviour):

P38: 8,2
Spit cw: 4,59
Ta152H: 8,8 :eek:

Power off stall speeds in Ah with the above settings:

P38L: 95-100mph(P38 manual say 100mph with a bit less weight, so thats rather ok)
Spit16: 70-80mph (Pilot notes say 95mph @ 3250kg)
Ta152H: 105mph.

If i compare this datas i would say in Ah they did install the airfoil of the Ta152H headover, or they did calculate it with the Spit16´s aspect ratio, while they took the Ta152H aspectratio to calculate the Spit16 lift.

This would explain why hte Ta152H perform the snap roll of a unstable wing-form and why the Spit16 stall rather smooth(at least in this relation).

This incredible high lift also explain the incredible energy management of the 16.

Greetings,

Knegel
Title: Re: Re: Spit 16
Post by: Ack-Ack on February 12, 2007, 02:58:59 PM
Quote
Originally posted by Serenity
It hovers. Its a UFO. It needs to be fixed.


You have film and accurate data to back up your claims?


ack-ack
Title: Spit 16
Post by: Ack-Ack on February 12, 2007, 02:59:51 PM
Quote
Originally posted by Serenity
Oh, and yeah. the Spixteen has issues, again in the vertical. THats where its screwed up.



Again, do you have any data to back your claims?


ack-ack
Title: Spit 16
Post by: Benny Moore on February 12, 2007, 03:41:19 PM
Quote
Originally posted by Knegel
I know fowlerflaps, but i never saw fowler flaps that double the liftfactor of a wing without to increase the drag dramatically, but thats what many flaps in AH do and thats why i call them "magic flaps".


The Fowler flaps do not double the lift on the P-38 in Aces High II, Herr Knegel, or anything like it.  Do some actual testing.

Quote
Originally posted by Knegel
Although the fowler flaps was more effective than most other systems, they dont made the P38 to a good sustained turning plane, like it is in AH!!


Yes, they did.  Without flaps, the P-38 out-turned the FW-190 and P-47, but with flaps it also out-turned the Me-109 and P-51.

Quote
Originally posted by Knegel
The P38 was know as a very good B&Z plane and the pilots wrote, "with help of the combat flaps, we could turn inside the smaler planes", to turn inside a plane dont mean to turn with it!!


The only country the fighters of which P-38s typically had to use the "boom-and-zoom" tactic against was Japan, because the Japanese had just about the most maneuverable fighters in the world.  Generally, all fighters had to use that tactic against Japanese crates, not just the P-38.  However, Standard U.S.A.A.F. tactics for the P-38 in Europe was dogfighting; specifically, P-38 pilots were instructed to - wait for it - use the Fowler flaps to out-turn the enemy.

Of course, that's a generalization.  There's a time and a place for everything.  Sometimes it was necessary to boom-and-zoom German planes, just as it was sometimes necessary for P-38s to turn fight with Zekes.  When doing the latter activity, they used maneuver flaps and sometimes even full flaps.
Title: Spit 16
Post by: Knegel on February 13, 2007, 12:21:47 AM
Hi Benny,

i dont know where you did read that the P38 pilots got introduced to make a close dogfight over europe, but thats absolut new to me.

What i most times read is that the P38 had bad problems in Europe, until the pilots did use B&Z tactics.

btw, the P38G in AH dont have fowler flaps!! At least the graphic show normal split flaps.

The P38 had a much to bad rollratio at slower speeds to make a effective dogfight. A systained turn dont mean the turnability in general, a sustained turn get much influenced by powerload and here the P38, like all other US planes was rather bad(actually so they are without flaps in AH).
Even the late P38J and L with 2 x 1600HP was rather poor in relation to the 109G10, G14 and K4, former versions was  even worse in relation to the german planes.

And again, the statement to be able to turn inside a plane dont mean to turn with it for longer time or to be able to make a good stallfight.

Actually the P38G flaps in AH double the turnperformence, they maybe dont double the lift, but they simply dont work like flaps should.

Without flaps it need roundabout 28sec to turn 360° at around 160mph in 4k alt.(thats actually what i would expect by a so underpowered plane)
With FULL flaps(full flaps have no "fowler effect" at all in any P38) it need 26sec for 360° at 105mph.  
The P38 maybe was able to fly with 105mph fully banked, but for sure it dont would turn faster than without flaps, simply cause the flaps create a very high drag.

Thats what i call "magical flaps"(F4U flaps work in the same way, maybe even more magical)!!

Greetings,


Knegel
Title: Spit 16
Post by: Ack-Ack on February 13, 2007, 01:06:15 AM
Quote
Originally posted by Knegel
Hi Benny,

i dont know where you did read that the P38 pilots got introduced to make a close dogfight over europe, but thats absolut new to me.

What i most times read is that the P38 had bad problems in Europe, until the pilots did use B&Z tactics.

btw, the P38G in AH dont have fowler flaps!! At least the graphic show normal split flaps.


Yes, the P-38G does have combat maneuvering/Fowler Flaps.  It doesn't have dive flaps, those didn't come until the late model J and L series.

Quote
The P38 had a much to bad rollratio at slower speeds to make a effective dogfight. A systained turn dont mean the turnability in general, a sustained turn get much influenced by powerload and here the P38, like all other US planes was rather bad(actually so they are without flaps in AH).
Even the late P38J and L with 2 x 1600HP was rather poor in relation to the 109G10, G14 and K4, former versions was  even worse in relation to the german planes.


True, the early model P-38s did have problems with the roll rate at medium to slow speeds but with the boosted ailerons that came in with the L series, that was alleviated somewhat.  However, at high speeds the P-38's roll rate was very good.

Quote
And again, the statement to be able to turn inside a plane dont mean to turn with it for longer time or to be able to make a good stallfight./quote]

I think a lot confuse the term "turn fighting" and actually think that it's just only a fight based around flat turns.  Most turn fighting engagements were angle fights, planes maneuvering for an angle and not necessarily using flat turns to gain the angle.  While the P-38 would be fodder against most planes in a flat turn fight, in an angles fight where the P-38 can use its flaps to gain an angle, the P-38 was quite capable in this regard.  Dan has posted a story of an engagement between some new pilots flying P-38Gs that got bounced on the deck by Bf109s and beat the German planes in an angles fight using their flaps.

Quote
Actually the P38G flaps in AH double the turnperformence, they maybe dont double the lift, but they simply dont work like flaps should.
[/b]

Since I've never flown a real P-38, I really can't say who the flaps were supposed to perform but from what I've read over the years, AH has it quite close, the only exception being the auto-retracting feature.

Quote
Without flaps it need roundabout 28sec to turn 360° at around 160mph in 4k alt.(thats actually what i would expect by a so underpowered plane)
With FULL flaps(full flaps have no "fowler effect" at all in any P38) it need 26sec for 360° at 105mph.  
The P38 maybe was able to fly with 105mph fully banked, but for sure it dont would turn faster than without flaps, simply cause the flaps create a very high drag.

Thats what i call "magical flaps"(F4U flaps work in the same way, maybe even more magical)!!


But the flaps in real life generated a nice amount of lift which in a turn fight can help make the turn a little tighter.  Here is an example, the P-38L had dive flaps that generated positive lift when deployed to aid in the recovery after a high speed dive.  P-38 pilots soon learned that you can also deploy the dive flaps during a high speed turn fight to help in high speed maneuvering.  And when they used the flaps, they only deployed them as needed and raised them afterwards.  So again, you're assuming that when a P-38 pilot uses flaps that he keeps them deployed the entire time.  I only use my flaps when needed and then raise them when I don't.  That's why if you watch any of my films you always hear the flaps moving.  I'm guessing the real P-38 pilots used the flaps the same way.


ack-ack

Greetings,


Knegel [/B]
Title: Spit 16
Post by: Karnak on February 13, 2007, 01:19:12 AM
Ack-Ack,

I understood that the boosted ailerons didn't help with low speed, where the pilot could just muscle maximum deflection, but only with high speed where the P-38s before the boosted ones really faired poorly.  The boosted ones roll great at speed, the unboosted ones roll terribly at speed.

That is how I understood it in anycase.
Title: Spit 16
Post by: Benny Moore on February 13, 2007, 07:43:27 AM
One thing to keep in mind is that the real P-38s had a lot more power, although we are talking about the early ratings we have in the game.  NACA data indicates that the boosted ailerons significantly improved roll rate at almost all speeds.  All P-38's from the P-38F-15 and onward had the maneuver flaps (but I believe they had Fowlers even before that).  It's the dive flaps that didn't appear until the P-38J-25.  Real Fowler flaps do improve turn time; they extend the wing area and therefore lower the wingloading, as well as providing all of the benefits of conventional flaps, and Fowlers cause no more drag than conventional flaps.  The P-38 does not, however, "double" its turning ability with flaps in the game.  As I said, it's not even close to that.  Fowler flaps should add about 40% more lift (30% more than conventional flaps, I believe, according to NACA).  The P-38 turns quite a bit less than 40% better (I'm not saying it should turn 40% better, as it's obviously a lot more complicated than that).  Lastly, if you've never read about P-38 pilots being told to out-turn the German fighters, you haven't done hardly any reading on the P-38.  The only situation where P-38s were not able to effectively dogfight with the Me-109 was at high altitude, where the engines did not put out enough power to make the maneuver flaps effective.  Below 20,000 feet, however, the two were very close in turning ability, with all of my sources giving the edge to the P-38 as long as it used the maneuver flaps.
Title: Spit 16
Post by: Knegel on February 14, 2007, 02:58:19 AM
Benny,

with FULL flaps(no fowler effect anymore), the P38 do this extreme turns!!

Full flaps of the P38 did cause a extreme nose down behaviour, high drag and more lift at slower speed, same like its in almost all planes!!

Specialy the nose down effect was needed to provide a better sight while landing.

In AH the F4U and P38 flaps (full flaps), work the other way around, they cause a incredible nose up behaviour, which, in combination with a banked plane, result in a very nice smooth tight turn, without the need to pull the elevator.

Such a behaviour simply is unreal, its magic!!

Full flaps are made to lower the stall speed and to provide a better sight(nose down) at same time, but the MUCH increased drag dont allow a increased turnrate with this setting!!


ITS MADE FOR LANDING!!

Even the P38 manual give the hint that the usage of the flaps make the plane nose heavy!!


Strangewise the fowler flaps (only the 1st steps work like fowler flap, afterward they pitch down like normal flaps) in AH dont work like fowler flaps. At higher speed with 1 step flaps, the turnrate dont improve, like it should.

But at slowspeed the turnrate improve and specialy the turnspeed get reduced by 35%.



Ack-Ack,

the boosted alerons mainly did help at highspeed, not at slow speed. All roll datas regarding the P38 i saw dont show a improved rollratio at slow speed.  At slow speed the pilot already was able to pull the stick to its maximum, so here was nothing to gain than a more light stick.

I know that the G should have the fowler flaps, but it looked to me that the AH G dont have them, now i had a look from a different angle, and closer distance and found they are displayed as fowler flaps.

But anyway, i talk about FULL flaps, not the normal manouver flap setting.


Greetings,

Knegel
Title: Spit 16
Post by: Benny Moore on February 14, 2007, 10:54:28 AM
That's better.  You now say 35% improvement in game instead of 200% improvement; that I can buy.  You're right that the real Fowler flaps were more efficient at the manuever extension than when fully deployed, but remember that they're still Fowlers.  Whether they're extended eight degrees (the maneuver setting) or fully deployed, the wing area of the wing is still greater than if the flaps were retracted.  That cannot be said of conventional flaps, which do not ever change the wing area.  Thus, the full flaps on the P-38 should be more effective than full flaps on an airplane with conventional flaps.  You may be right that full flaps are too effective in turning - I've often wondered this myself.  However, if that is so, it is true of all ships in the game, not just the P-38.

Where did you hear that the full flaps on the P-38 caused a nose down pitching movement?  I've never found any such statement in either the Pilots Manual for the Lockheed P-38 Lightning or the Pilot Training Manual for the Lockheed P-38 Lightning.  However, even if it does (not unbelieve as flaps can cause nose down pitching in some airplanes), that doesn't mean it affects the sustained turning ability.  The dive flaps ("airbrakes") caused a nose up pictchig movement (which pilots did use to their advantage in short-term turns, usually when leading a target); but would this create a better sustained turn?  I doubt it.  Nose down pitch from flaps should not mean the airplane turns worse sustained any more than nose up pitch from the dive flaps makes the ship turn better sustained.

I do know that some P-38 pilots used full flaps when turn fighting Zekes, so it must have provided at least a marginal improvement over the maneuver setting (at the expense of speed, of course).  Was it a recommended tactic?  Of course not, but sometimes you don't have a choice.  Point is, it allowed the pilot do do something he could not with the maneuver flap setting.  And the pilots manual states that it's impossible to strike the tail on the ground unless full flaps are deployed.  This clearly means that, for the real P-38, a higher angle of attack is possible with full flaps than without.  Objectively, I must also point out that it does indicate that the Aces High P-38 may be able to pull too high of an angle of attack near the stall speed when the flaps are not deployed; in Aces High, the P-38 can strike its tail on the ground even with flaps fully retracted, at military power as well as at war emergency power.  Fuel load does not seem to have a bearing on this.

As for the roll rate, I believe you're again wrong.  I have a chart created by an associate from NACA data; he's a FW-190 fanatic and not a P-38 nut, so you need not fear American bias.  I am not sure of the reason for the discrepancy in P-38 roll rates at slow speed.

(http://users.adelphia.net/~j.r.engdahl/josh/Roll%20chart.jpg)

By the way, according to German Me-109 aces, the Me-109 versus P-38 situation was the exact opposite of what you say.  You say that the P-38 might turn better instantaneously but the Me-109 should turn better sustained; German aces, however, said that the Me-109 turned better in the short term but the P-38 would catch up as the speeds went down.  They advocated never flat turning with a P-38 but rather changing directions often, taking advantage of the P-38's relatively poor roll rate.  This was, of course, before the boosted ailerons.
Title: Spit 16
Post by: Benny Moore on February 14, 2007, 11:36:48 AM
I just did a few calculations based on Dokgonzo's and Mosq's testing at Netaces.  I have no idea what calculations and tests you're using, Knegel, because here's what I got.

Turn radius:
Me-109F-4 with full flaps has 74% of the radius of a no flap turn.
Me-109G-2 with full flaps has 73% of the radius of a no flap turn.
Me-109G-14 with full flaps has 73% of the radius of a no flap turn.
Me-109K with full flaps has 75% of the radius of a no flap turn.
P-38G with full flaps has 73% of the radius of a no flap turn.
P-38L with full flaps has 73% of the radius of a no flap turn.

Turn time:
P-38L with full flaps has 94% of the turn time of a no flap turn.
Me-109K with full flaps has 99% of the turn time of a no flap turn.

According to these caculations, the improvement in turn radius that full flaps give the P-38 is no more than what the Me-109 gets, and the improvement in turn time that full flaps give the P-38 is only 5% better than that of the Me-109.  Since real Fowlers give 30% more lift than conventional flaps, I don't think a Fowler-equipped ship having a 5% improvement over a crate with conventional flaps in a full flap turn is an unreasonable figure.

However, it appears that full flaps are indeed too effective in Aces High II, for both flap types.  According to Mosq's tests, full flaps improve the turn times for both the P-38 and the Me-109.  In reality, only Fowlers could possibly improve turn times (and even then I doubt that they would if they're fully deployed).  By all sources, conventional flaps should hurt the turn time, only giving a benefit in turn radius.

P.S.  Mosq's tests are not standard sustained turn tests.  However, judging by his method description, the results should not be off by more than a few percent.  If you have a better set of tests, by all means direct me to them.
Title: Spit 16
Post by: Guppy35 on February 14, 2007, 11:52:16 AM
Quote
Originally posted by Serenity
Oh, and yeah. the Spixteen has issues, again in the vertical. THats where its screwed up. Its VERY easy to kill. It really is. Any turn fighter, and any P-40E can easily incinerate one. Just never challenge it in the vertical. Thats why the kill stats are down. n00bs TnB, and thats where they get eaten. As soon as they learn to climb they are unstoppable.

lol Guppy. Im not so sure. Im more afraid of mk IXs than spixteens, because the only ones who fly the mk IX, are the ones who know how to fight. The same WOULD go for the V, but I know a lot of n00bs who are knowlageable (Yeah, I spelled that wrong, its been a long day) enough to recognize the V, and have been warned not to fly the Spixteen then go to Vs and are again baby seals. There are many more good pilots in mk Vs than in XVIs, I find. Id like to see the XVIe though. The non-clipped. Im curious as to if it too would be a UFO here.


Here we go with its the plane not the pilot again.  Someone knows how to work it so it must be a UFO.

I'm average at best and I'm 13-1 vs the 16 in my 38G and I go vertical with em all the time.  I'm 30-2 vs Spits in general.

So does that mean my 38G is more uber or do maybe I just know how to use my 38G fairly well?

You guys want to change a flight model because you've run up against someone who can clean your clock in a Spit 16.

Ya know what?  I have run up against those guys too.  Stang can, FX1 can to name a couple.  I've not reached their level of ability so they eat me up.

They can take the good qualities of the 16 and add their skill and it's just about unbeatable.

But it's not a UFO.
Title: Spit 16
Post by: FX1 on February 14, 2007, 12:37:46 PM
The 16 just like any other plane it has disadvantages. Its not a super plane by any means. What the 16 is good at is vert fighting. The 16 disadvantage is fighting nose down. I never really have a problem with that because i fight at low alt and only use alt advantage if capping a field.

I think the 16 gets a bad name because people dont understand that a 16 can go from the deck to 6k nose up. People get picked our try and bnz with a 16 and you just cant do it under 10k.

A newb in a 16 is a newb in a nikki so on. I have never had a problem fighting the 16 because i understand its flight characteristics. A good pilot in a 38 can kill a newb in a 16 9/10 times.

You know at one point i hated the la7 reallllly disliked the plane. Called people la la dweeb and everything under the sun. Then as i got better i started to perfect my overshoots and guess what i dont have a problem with the LA anymore. Hell i will fly one a couple times each camp to get a feel for it.


BTW the F4u's will eat a 16 today in AH.

Today i fly the f4ua1 and f4u4 because it is the most dominant plane in the game.
Title: Spit 16
Post by: Ack-Ack on February 14, 2007, 12:42:18 PM
Quote
Originally posted by Guppy35
Here we go with its the plane not the pilot again.  Someone knows how to work it so it must be a UFO.

I'm average at best and I'm 13-1 vs the 16 in my 38G and I go vertical with em all the time.  I'm 30-2 vs Spits in general.

So does that mean my 38G is more uber or do maybe I just know how to use my 38G fairly well?

You guys want to change a flight model because you've run up against someone who can clean your clock in a Spit 16.

Ya know what?  I have run up against those guys too.  Stang can, FX1 can to name a couple.  I've not reached their level of ability so they eat me up.

They can take the good qualities of the 16 and add their skill and it's just about unbeatable.

But it's not a UFO.


But damnit Dan, he saw this on the History Channel and he's got back seat time in a glider!  And even though he's never flown the Spitfire XVI in game, he knows all about the flight model and how its was supposed to be because he watched the Battle of Britain on late night TV!


ack-ack
Title: Spit 16
Post by: Bronk on February 14, 2007, 12:46:48 PM
Quote
Originally posted by Ack-Ack
But damnit Dan, he saw this on the History Channel and he's got back seat time in a glider!  And even though he's never flown the Spitfire XVI in game, he knows all about the flight model and how its was supposed to be because he watched the Battle of Britain on late night TV!


ack-ack


Don't forget his hundreds of game films Ack-Ack.


Bronk
Title: Spit 16
Post by: FX1 on February 14, 2007, 12:54:14 PM
Also the 16 can turn very well you just need to understand the throttle to get the most out of the plane.
Title: Spit 16
Post by: Knegel on February 15, 2007, 02:21:07 AM
Hi Benny,

you be right regarding the flaps of other planes in AH, and i must say iam shocked!!

I rarely did use the flaps of the 109´s and 190´s and Spit´s for now, cause iam used to lose turnperformence by them, but since one of the lasts patches it seems that all planes got this magical flaps.
You be absolut right that normal flaps shouldnt result in a turnrate gain, at least not at max position!

Oh my god, this turn AH to be a arcade game.  :mad:

btw, the turn radius of the P38G with full flaps is 194m, without flaps its  around 320m.  The lift gain by full flaps must be by around 100% to archive this!!

And now most, if not, all planes behave like this.  :cry

Also the 109K now turn full banked with full flaps 5mph above stallspeed, big balloons would have such a effect, but not flaps. :furious

If a plane stall out in a strait flight at 100mph, where does the lift comes from to keep a level turn with 45° or more banking angle at 105-110mph??

Afaik while a horizontal turn with a 45° bank angle,  the lift force get shared in 50% upward and 50% toward the  turn center, to be able to keep a horizontal turn with 45° bank, there is a lift increasement of 100% needed!! And that within 5-10mph?? :noid

Thats what i call magic!!


Greetings,

Knegel
Title: Spit 16
Post by: Benny Moore on February 15, 2007, 07:31:44 AM
It does explain why my efforts to turn at best sustained turn speed are always foiled by someone turning with full flaps.  It frustrates me to be forced to go to full flaps; I don't mind using full flaps, as real pilots did it sometimes, but it should not be more efficient than turning at best turn speed.  The result should most probably be a temporary gain which would hurt you in the long run if you didn't make your shot.

However, before I state with certainty that the modelling is wrong, I need to find a better set of tests.  Mosq's test method is somewhat questionable; for one thing, he doesn't quite turn at the best turn speed when not using flaps.  There is a possibility that the results are skewed as a result.
Title: Spit 16
Post by: Bronk on February 15, 2007, 08:38:24 AM
Quote
Originally posted by Knegel
Snip


You want uber flappen fest Fly the IL2 series.

There my friend is where the magic flaps are.

Bronk
Title: Spit 16
Post by: Kweassa on February 15, 2007, 10:25:32 AM
Just wait a moment, Knegel.

 I feel a bit awkward here, because I generally agree to the premise that some planes are just too efficient with their usage of flaps, particularly the heavier US 'Pursuit' birds and Navy/Marine planes. However I don't think what you are saying can be just generalized as it is.

 For example;

Quote
I rarely did use the flaps of the 109s and 190s and Spits for now, cause iam used to lose turnperformence by them, but since one of the lasts patches it seems that all planes got this magical flaps.


 Statements like these are extremely questionable because under the same circumstances my 'feel' is entirely different from yours.

 For example, the 109s in particular have received a very slight raise in accessible speeds where the first notch of flaps are allowed with the last few versions, however flying the 109 almost exclusively for many years I've never really felt that they truly increased the turn rate. The most obvious use for flaps when combating (for example) a US plane in the 109s is when the enemy pilot knows what he is doing. He engages in a series of very harsh vertical maneuvers leading into a rolling scissors situation which is incredibly difficult to follow for a German bird, because the stability factor kicks in very hard for the 109. When the plane is forced into high AoA the roll axis stability decreases dramatically, and only with the use of flaps can the 109 be stabilized enough to follow the enemy plane throughout the maneuver. In those situations the 109 pilot is forced to engage flaps despite its detrimental effect to speed. It is not because he wants the 109 to "turn better", but simply because it is a necessity to stabilize the plane.

 The same holds for the 190s and 109s. The plane seems to turn better, but not truly better as some do. It simply allows the plane stabilize better, which makes it "easier to turn harder", as opposed to truly "turn better". The 109s and 190s were always like that.


Quote
You be absolut right that normal flaps shouldnt result in a turnrate gain, at least not at max position!

Oh my god, this turn AH to be a arcade game.  

btw, the turn radius of the P38G with full flaps is 194m, without flaps its around 320m. The lift gain by full flaps must be by around 100% to archive this!!

And now most, if not, all planes behave like this.  


 Here I notice a strange confusion, if not yours at least on my part. Why do you equate the concept of "smaller turn radius" with "better turn rate"?

 Those two concepts are sometimes joined but in many cases far apart. A plane may be able to turn extremely tight, but at the expense of turn speed and efficiency. Most combat situations validate the importance of the "turn radius" as opposed to the "turn rate", and I can see why some people may consider this as "turning better", as a loose expression of explaining the situation. However, just because a plane has engaged into an extremely tight turn, utilizing fully extended flaps, it doesn't automatically mean that plane is truly "turning at a better rate".

 The P-38 may be able to turn at a 320m radius with flaps up at a certain speed and certain power setting. If he engages full flaps, the stability of the plane will go up, the stall speed goes down, and he will be able to keep the plane in a state of very high AoA which will make it turn at a 194m radius, but at a considerably slower speed in exchange. Is this really so unbelievable? For one thing, I don't consider this situation as the "P-38 gaining a better turn rate". I consider it "P-38 gaining a tighter turn radius"[/u].


Quote
Also the 109K now turn full banked with full flaps 5mph above stallspeed, big balloons would have such a effect, but not flaps.  

If a plane stall out in a strait flight at 100mph, where does the lift comes from to keep a level turn with 45?or more banking angle at 105-110mph??


 From the camber, and the subsequent stabilizing effect.

 Having full flaps out doesn't necessarily mean the lift from the plane will be gone. It merely means the drag caused by the flaps is so high that the additional lift provided by the high flap angle cannot compensate for the drag. At that point, when the plane goes over the 'equilibrium' the drag overcomes all lift, the speed drops considerably, and the plane will "mush" into a stall. However, my take is that it is entirely possible for a plane with high power loading and tremendous engine power, to keep it at a better state of extreme turning even with very high flap angles. After all, turning is a horizontal climb. The more power, the better the plane can compensate for the drag.

 One good comparison might be the Spitfires in the game. At least, in my own experience, using the flaps in the Spitfires are almost a 'last resort' manuever. If the situation calls for me to try and turn this already tight-turning plane even tighter, then I will momentarily drop flaps down and then immediately bring them back up. To me, the plane doesn't feel like it is actually "turning better". In a last-resort attempt to turn the Spit as tight as possible, I will let the flaps deflect down maximum angle - and when that happens, it only feels like turning tighter, not turning better. The speed is so low that there is considerable amount of anxiety in regards to the plane just 'mushing down' out of control.

 Clearly, to me, this is an indicator the flaps are working as they should. Full flaps are warranted only when the importance of an absolutely smaller turning radius greatly outweighs the importance of generally better turn rate. Only in those situations where both you and the enemy are locked into a dead-heat turning contest, where giving even the slightest ground to the other will result in giving him a gun solution, do we really need to go into full flaps, even if we are loathe to do it (since being locked into a duel that requires full-flaps to win, means you are totally committed to that fight where only one of you will walk out alive).

 
Quote
Afaik while a horizontal turn with a 45?bank angle, the lift force get shared in 50% upward and 50% toward the turn center, to be able to keep a horizontal turn with 45?bank, there is a lift increasement of 100% needed!! And that within 5-10mph??  

Thats what i call magic!!

 
 Not if that '100%' is already within the limits of the plane. I'm no expert in aerodynamical physics so this is but a speculation, but IMO your analogy would only be correct when a plane has only enough lift to keep the plane just level. This would mean the comparative ratio of drag to excess thrust would be 1 : 1, or only slightly in favor of the thrust (not withstanding the amount of thrust already required to move the plane forward in the first place). Then the plane would produce just enough speed to fly level, and therefore, if it goes into a 45d bank angle, there would be no way to flat-turn the plane without losing alt.

 However, what if the plane has an engine already powerful enough to produce the amount of lift required to turn the plane, without having to lose alt at all?

 I'm sure those who are better educated in aerodynamics could offer a better explanation, but even to me your analogy of this 'magic' seems a little strange.
Title: Spit 16
Post by: Benny Moore on February 15, 2007, 10:58:11 AM
Kweassa, the problem is that using full flaps in Aces High II does result in an improved turn time and not just an improved turn radius.  That is if Mosq's test results are correct, which I am unsure.  If using full flaps improves turn radius but degrades turn time, then it is as it should be.  If, however, conventional flaps are improving both turn radius and turn time, then there is a big problem.

Also, you may have missed my statement about the numbers.  According to the numbers, the Me-109 and FW-190 get the same turn radius benefit from using full flaps as the P-38 and P-47, and a lot more than the P-51.  So I don't know what you mean about "too efficient with their usage of flaps, particularly the heavier U.S. birds."  The F4U, of course, is the exception, and I would agree fully that something's fishy about it.
Title: Spit 16
Post by: Kweassa on February 15, 2007, 02:47:38 PM
Quote
Kweassa, the problem is that using full flaps in Aces High II does result in an improved turn time and not just an improved turn radius. That is if Mosq's test results are correct, which I am unsure. If using full flaps improves turn radius but degrades turn time, then it is as it should be. If, however, conventional flaps are improving both turn radius and turn time, then there is a big problem.


 Benny, a "turn rate" is the ratio of the circular angle travelled during a turn in accordance to time it has taken. A direct comparison of turn rate is only meaningful when the plane travels the same distance.

 If a plane flies without flaps at a certain turn rate, and then it flies the exact same course again at the same power setting (but with full flaps engaged this time), and the results show a better turn rate, then something is clearly wrong. However, when a plane engages full flaps the turn radius is minimalized. And therefore, this turn rate cannot be compared with the turn rate of the plane flying at a larger radius.

 A turn rate is calculated at degrees/second =  360 / ( ( 2 x pi x r ) / v )

 Therefore the turn rate is in inverse proportion to the radius barring the effect of the plane's speed. A smaller turn radius automatically means a better turn rate, unless the turning speed becomes sufficiently low enough to actually cut down the entire turn rate. If the speed difference is not enough, or in other words, if a certain plane has so much excess power that the plane is able to hold a certain amount of speed despite the great drag increase caused by flaps, then even with full flaps engaged the plane will show a better turn rate because it is travelling a considerably shorter distance at a comparable time.

 In a general sense, it would seem that the more powerful, late-war aircraft with better power loading and lots of excess thrust will typically show a better turn rate even when using high flap deflection, but an early war aircraft with a relative worse power loading should show worse turn rate when high flap deflection is used. If there is one thing for certain, it is not impossible to have a bette turn rate despite full flaps. It is a matter of the individual plane.

(contd.)
Title: Spit 16
Post by: Kweassa on February 15, 2007, 02:48:15 PM
(contd.)

 Another key factor in this discussion that must be brought up, is the possibility that the initial tests might be wrong or inadequate. Take for example the data extracted by my own testings. This data is a few versions old so absolute accuract cannot be guaranteed, but it will show as an example that different sets of data may be reached by different testers.

......




Quote
-Results Format-

Type (SL angle used)
- time to complete under normal setting (average turn speed), radius
- time to complete under one notch of flap (average turn speed), radius
- time to complete under full flap (average turn speed), radius

*Individual Notes




A6M2 (0.05)
- 14 seconds (123mph), 122.3m
- 14 seconds (115mph), 114.5m
- 14 seconds (105mph), 104.6m


A6M5b (0.05)
- 15 seconds (130mph), 138.7m
- 14 seconds (125mph), 124.5m
- 15 seconds (108mph), 115.3m


Bf109E-4 (1.0/1.1/1.2)
- 17 seconds (152mph), 183.9m
- 18 seconds (138mph), 176.8m
- 18 seconds (118mph), 151.1m


Bf109F-4 (1.0/1.2/1.2)
- 16 seconds (162mph), 184.5m
- 18 seconds (146mph), 187.1m
- 18 seconds (138mph), 175.5m


Bf109G-2 (1.0/1.2/1.2)
- 17 seconds (167mph), 202.1m
- 18 seconds (160mph), 205.0m
- 17 seconds (148mph), 179.0m


Bf109G-6 (1.0/1.2/1.2)
MG151/20
- 18 seconds (163mph), 208.8m
- 18 seconds (160mph), 204.9m
- 18 seconds (134mph), 171.6m
MK108
- 18 seconds (168mph), 215.2m
- 19 seconds (158mph), 213.6m
- 18 seconds (137mph), 175.5m


Bf109G-10 (1.0/1.3/1.3)
MG151/20
- 18 seconds (176mph), 225.5m
- 19 seconds (163mph), 220.4m
- 19 seconds (142mph), 192.0m
MK108
- 18 seconds (179mph), 229.3m
- 19 seconds (167mph), 225.8m
- 19 seconds (149mph), 201.5m


Bf110C-4 (0.05)
- 20 seconds (139mph), 197.8m
- 19 seconds (119mph), 161.0m
- 16 seconds (100mph), 142.3m


Bf110G-2 (1.0)
- 22 seconds (145mph), 227.0m
- 22 seconds (131mph), 205.1m
- 20 seconds (105mph), 149.5m


C.202 (0.05)
- 20 seconds (142mph), 202.1m
- 18 seconds (146mph), 187.0m
- 18 seconds (129mph), 165.2m


C.205 (1.0)
- 19 seconds (168mph), 227.2m
- 18 seconds (162mph), 207.5m
- 20 seconds (136mph), 193.6m


F4F-4 (0.05)
- 21 seconds (125mph), 186.8m
- 20 seconds (118mph), 167.9m
- 20 seconds (98mph ), 139.5m


FM-2 (0.05)
- 18 seconds (133mph), 170.4m
- 16 seconds (129mph), 146.9m
- 18 seconds (100mph), 128.1m


F4U-1 (1.0)
- 20 seconds (154mph), 219.2m
- 21 seconds (138mph), 206.2m
- 20 seconds (106mph), 150.9m


F4U-1D (1.0)
- 19 seconds (160mph), 216.4m
- 19 seconds (149mph), 201.5m
- 19 seconds (110mph), 148.7m


F4U-1C (1.0)
- 21 seconds (162mph), 242.1m
- 20 seconds (150mph), 213.5m
- 20 seconds (110mph), 156.6m


F4U-4 (1.0)
- 19 seconds (168mph), 227.2m
- 18 seconds (162mph), 207.5m
- 18 seconds (113mph), 144.7m


F6F-5 (1.0)
- 20 seconds (160mph), 227.7m
- 19 seconds (145mph), 196.1m
- 19 seconds (118mph), 159.5m


Fw190A-5 (1.0/1.5)
- 21 seconds (180mph), 269.0m
- 21 seconds (162mph), 242.1m
- N/A

Fw190A-8 (1.0/1.5)
4xMG151/20
- 23 seconds (181mph), 296.3m
- 21 seconds (171mph), 255.6m
- N/A
2xMG151/20, 2xMK108
- 23 seconds (181mph), 296.3m
- 23 seconds (172mph), 281.6m
- N/A


Fw190D-9 (1.0/1.5)
- 22 seconds (181mph), 283.4m
- 21 seconds (172mph), 257.1m
- N/A


Fw190F-8 (1.0/1.5)
- 23 seconds (179mph), 293.0m
- 22 seconds (171mph), 267.8m
- N/A

* Fw190s cannot maintain a turn tight/slow enough for full flaps


Hurricane Mk.Ia (0.05)
- 15 seconds (126mph), 134.5m
- N/A
- 15 seconds (104mph), 111.0m


Hurricane Mk.IIc (0.05)
- 15 seconds (136mph), 145.2m
- N/A
- 15 seconds (116mph), 123.8m


Hurricane Mk.IId (0.05)
- 16 seconds (146mph), 166.2m
- N/A
- 17 seconds (116mph), 140.3m

* Hurricanes and Spitfires have only landing flap positions available


Ki-61-I-Tei (0.05)
- 18 seconds (151mph), 193.4m
- 18 seconds (146mph), 187.0m
- 19 seconds (131mph), 177.1m


Ki-84-I-Ko (0.05)
- 17 seconds (153mph), 185.1m
- 17 seconds (130mph), 157.3m
- 16 seconds (117mph), 133.2m


La-5FN (0.05)
- 18 seconds (156mph), 199.8m
- 17 seconds (150mph), 181.5m
- 17 seconds (126mph), 152.4m


La-7 (0.05)
ShVAK
- 18 seconds (162mph), 207.5m
- 18 seconds (153mph), 196.0m
- 17 seconds (127mph), 153.6m
B-20
- 18 seconds (162mph), 207.5m
- 17 seconds (151mph), 182.7m
- 17 seconds (126mph), 152.4m


Me163B (0.05)
- 17 seconds (210mph), 254.1m
- 17 seconds (196mph), 237.1m
- N/A

* Me163B flies too fast at full throttle turn, for full flaps to be used


Me262A (0.05)
- 27 seconds (204mph), 392.0m
- 28 seconds (190mph), 378.7m
- 31 seconds (153mph), 359.6m


Mosquito Mk.VI (0.05)
- 21 seconds (149mph), 222.7m
- 18 seconds (140mph), 179.3m
- 20 seconds (118mph), 167.9m


N1K2-J (0.05)
- 17 seconds (167mph), 202.0m
- 16 seconds (153mph), 174.2m
- 15 seconds (134mph), 143.0m


P-38G (0.05)
- 19 seconds (174mph), 235.3m
- 20 seconds (157mph), 223.5m
- 18 seconds (116mph), 148.6m


P-38J (0.05)
- 21 seconds (180mph), 269.0m
- 19 seconds (170mph), 229.9m
- 19 seconds (116mph), 156.8m


P-38L (0.05)
- 21 seconds (184mph), 275.0m
- 19 seconds (169mph), 228.5m
- 19 seconds (119mph), 160.9m


P-40B (1.0)
- 21 seconds (139mph), 207.7m
- 21 seconds (131mph), 195.8m
- 21 seconds (112mph), 167.4m


P-40E (1.0)
- 19 seconds (154mph), 208.2m
- 19 seconds (140mph), 189.3m
- 19 seconds (124mph), 167.7m


P-47D-11 (0.05)
- 23 seconds (153mph), 250.5m
- 23 seconds (136mph), 222.6m
- 22 seconds (120mph), 187.9m


P-47D-25 (0.05)
- 23 seconds (157mph), 257.0m
- 23 seconds (143mph), 234.1m
- 23 seconds (120mph), 196.4m


P-47D-40 (0.05)
- 24 seconds (159mph), 271.6m
- 22 seconds (151mph), 236.4m
- 23 seconds (124mph), 203.0m


P-51B (0.05)
- 23 seconds (149mph), 243.9m
- 21 seconds (143mph), 213.7m
- 23 seconds (118mph), 193.1m


P-51D (0.05)
- 23 seconds (158mph), 258.6m
- 21 seconds (150mph), 224.2m
- 22 seconds (121mph), 189.4m


Spitfire Mk.Ia (0.05)
- 17 seconds (117mph), 141.5m
- N/A
- 17 seconds (97mph) , 117.3m


Spitfire Mk.V
- 16 seconds (137mph), 156.0m
- N/A
- 17 seconds (105mph), 134.5m


Seafire Mk.II (0.05)
- 16 seconds (140mph), 159.4m
- N/A
- 18 seconds (106mph), 135.8m


Spitfire Mk.IX (0.05)
30cal
- 16 seconds (144mph), 164.0m
- N/A
- 16 seconds (118mph), 134.3m
50cal
- 17 seconds (141mph), 170.6m
- N/A
- 17 seconds (121mph), 146.4m


Spitfire Mk.XIV (0.05)
30cal
- 16 seconds (165mph), 187.9m
- N/A
- 18 seconds (119mph), 152.4m
50cal
- 17 seconds (166mph), 200.8m
- N/A
- 18 seconds (118mph), 151.1m


Ta152H-1 (1.0)
- 20 seconds (184mph), 261.9m
- 20 seconds (173mph), 246.2m
- N/A

* Ta152 cannot maintain a turn tight/slow enough for full flaps


Typhoon Mk.Ib (0.05)
- 20 seconds (163mph), 232.0m
- N/A
- N/A


Tempest Mk.V (0.05)
- 18 seconds (168mph), 215.2m
- N/A
- N/A

*Typhoon and Tempest flies too fast at full throttle turn, for flaps to be used


Yak-9T (0,05)
- 20 seconds (144mph), 205.0m
- 19 seconds (132mph), 178.5m
- 19 seconds (116mph), 156.8m


Yak-9U (0.05m)
- 19 seconds (152mph), 205.5m
- 18 seconds (144mph), 184.5m
- 19 seconds (129mph), 174.4m



 ...

 Out of 53 plane types, 20 planes are recorded as having a better turn rate at full flaps. However the differences in turn times are hardly more than 1~2 seconds apart in each ase. The majority of the planes either have a worse off turn rate, or basically an unchanged turn rate when turning with full flaps. Some of them can't even fly a turn tight/slow enough to use full flaps in a full 360d turn in the first place.

 The list of the planes that have a better turn rate at full flaps is as follows;

Bf110C-4
Bf110G-2
C.202
F4F-4
F4U-1C
F4U-4
F6F-5
Ki-84-I-Ko
La-5FN
La-7
Mosquito Mk.VI
N1K2-J
P-38G
P-38J
P-38L
P-47D-11
P-47D-40
P-51D
Spitfire Mk.V
Yak-9T


 Some of them are strange, but other are as expected.

 For instance, the Ki-84 has an even more efficient Fowler flap layout than the P-38s. The N1K2 is a very well handlong plane equipped with an automatically engaged combat flap system. The Soviet Lavochkin fighters are among the best accelerating planes in the game, and all your precious P-38s have also made it in the list.

 On the contrary, all the Spitfires have a one-stage flap that deploys fully at a very extreme angle. As you can see only the Spit5 made it into the list, and all the rest of the Spits show a worse off turn rate at full flaps.

 The 110s or Macchi fighters are quite a surprise, but what's even more surprising is the number of US fighters on the list. Almost all of them have show a better turn rate with full flaps engaged.



 In conclusion, aside from a few unexpected anomalies (and extremely suspicious situation concerning US fighters using highly deflected flap settings), most of the fighters do have a worse turn rate with full flaps. Knegel's comment, at least from my point of view, is either a clear exaggeration of what's really going, or a misinformation from questionable test data, or maybe even both.
Title: Spit 16
Post by: Widewing on February 15, 2007, 06:33:34 PM
Quote
Originally posted by Kweassa
(contd.)

 Bf109F-4 (1.0/1.2/1.2)
- 16 seconds (162mph), 184.5m
- 18 seconds (146mph), 187.1m
- 18 seconds (138mph), 175.5m


 Out of 53 plane types, 20 planes are recorded as having a better turn rate at full flaps. However the differences in turn times are hardly more than 1~2 seconds apart in each ase. The majority of the planes either have a worse off turn rate, or basically an unchanged turn rate when turning with full flaps. Some of them can't even fly a turn tight/slow enough to use full flaps in a full 360d turn in the first place.

 The list of the planes that have a better turn rate at full flaps is as follows;

Bf110C-4
Bf110G-2
C.202
F4F-4
F4U-1C
F4U-4
F6F-5
Ki-84-I-Ko
La-5FN
La-7
Mosquito Mk.VI
N1K2-J
P-38G
P-38J
P-38L
P-47D-11
P-47D-40
P-51D
Spitfire Mk.V
Yak-9T


 Some of them are strange, but other are as expected.

 For instance, the Ki-84 has an even more efficient Fowler flap layout than the P-38s. The N1K2 is a very well handlong plane equipped with an automatically engaged combat flap system. The Soviet Lavochkin fighters are among the best accelerating planes in the game, and all your precious P-38s have also made it in the list.

 On the contrary, all the Spitfires have a one-stage flap that deploys fully at a very extreme angle. As you can see only the Spit5 made it into the list, and all the rest of the Spits show a worse off turn rate at full flaps.

 The 110s or Macchi fighters are quite a surprise, but what's even more surprising is the number of US fighters on the list. Almost all of them have show a better turn rate with full flaps engaged.



 In conclusion, aside from a few unexpected anomalies (and extremely suspicious situation concerning US fighters using highly deflected flap settings), most of the fighters do have a worse turn rate with full flaps. Knegel's comment, at least from my point of view, is either a clear exaggeration of what's really going, or a misinformation from questionable test data, or maybe even both. [/B]


Kweassa, That is old data taken well before the major changes in the drag model.

In many if not all instances, things have changed. I suggest you re-test the aircraft some day and compare the old data to the current flight model.

My regards,

Widewing
Title: Spit 16
Post by: Kweassa on February 15, 2007, 06:49:04 PM
Quote
Kweassa, That is old data taken well before the major changes in the drag model.

In many if not all instances, things have changed. I suggest you re-test the aircraft some day and compare the old data to the current flight model.


 I am aware of that WW, I was just trying to make a point that some planes were always showing a slightly better turn rate at full flaps, and it wasn't such a strange thing to see.

 The recent drag model change is said to have penalized planes even more severely when at high flap deflection (according to HT), so if any new testing is done on my part I'd expect the turn rate at full flaps getting even worse.
Title: Spit 16
Post by: Knegel on February 16, 2007, 01:44:03 AM
Hi  Kweassa,

i had exact your datas in mind when i started this discussion!!

What you write regarding the roll instability and the need to flaps to stabilize the plane, with the knowledge that the turnrate dont increase is how it was!!

At that time(your tests show that) only some planes had the "magical flaps"(i found the P51D, F4U and P38 took most and unbelievable benifit by full flaps, but i also found the 190A flaps much to good, while the 190 had many problems otherwise, so this benefit didnt show up that much)

Now also the 109´s turnmuch better with full flaps!!

The turnrate remain rather the same, but the radius decrease extreme, similar to the F4U and P38!!

Take a 109K, 100% fuel, then seak for the slowest speed in a level flight without altitude lost(full flaps), thats around 95-100mph. At this speed its of course impossible to bank the plane without altlost, cause we need 100% lift to keep alt.

But already at 105-110mph we can make the most tight turn with a 45° bank.

So we gain 100% lift within 5-15mph!!

Isnt that magic??

At least we dont need to complain the US flaps anymore. lol

Normal flaps dont increase the lift in general!!

In most planes flaps decrease the max lift!!

Flaps shift the speed of best lift to a slower speed and they specialy lower the nose of the plane while that, but at same time the max AoA get decreased as well and this have in many cases a smaler lift as result.

You need to understand why this is so:

Most planes can fly below landing speed without flaps, , the problem is that the angle of attack in this flightposition would let touch the tailwheel at 1st and of course the pilot would have problems to see the runway.

Full flaps now change the airfoil, its somewhat like the whole wing turned around, to have a more big angle in relation to the flightdirection.

As result the wing get a higher AoA  when the flaps get extracted, without to move the elevator,  but the airfoil dont allow a that high max AoA anymore.

The changed airfoil would explain the upmoving nose for some time, on the other had the full extended flaps cause a asymetrical drag below the plane, somewhat a leverage and as faster the plane fly this leverage will push the nose down.
The rather bad formed extreme slowspeed airfoil(wing + full flaps) will lose its lift at higher speeds rather fast, cause the airflow will break, so the drag leverage of the flaps will move the nose down.

Flaps only change the Airfoil from a highspeed to a slow speed airfoil, while the wingarea DECREASE.  
So we have at one stage a very smooth airfoil with a bigger wingarea and on the other had a pretty squary airfoil with a smaler wingarea.

Real flaps rarely will increase the turnradius in a sustained turn, neighter the turn ratio!!

The high drag of the full extended flaps in combination with the smaler max lift make a turn radius gain while a sustained turn, like we have it now in AH, almost impossible.

Greetings,

Knegel
Title: Spit 16
Post by: Krusty on February 16, 2007, 10:55:55 AM
Knegel, you're saying you need 100% more lift to bank 45 degrees. You don't. You can bank 45 degrees without flaps and not fall from the sky.
Title: Spit 16
Post by: squealer on February 16, 2007, 11:48:00 AM
turns inside a zero
speed of a tempest

You talk bollocks, on both accounts...
Title: Spit 16
Post by: Benny Moore on February 17, 2007, 12:37:42 PM
Kweassa, I am certain that what you describe is impossible with conventional flaps.  If that were the case, it would be advantageous to take off with full flaps.  In reality, if two conventional flap ships take off simulataneously and one uses flaps and the other does not, the airplane using flaps will take off first.  However, a minute later, the airplane that did not use flaps will be higher and faster, even if the ship that used flaps raised them soon after takeoff.

That is not the case in reality.  Aircraft handbooks universally recommend taking off without flaps unless the runway is short or an obstacle must be cleared.  This is because conventional flaps are much less efficient than not using flaps.  For the same reason, using conventional flaps to turn should decrease the turn radius but increase the turn time.  Fowler flaps are another story because they increase wing area, thus lowering wingloading.
Title: Spit 16
Post by: Knegel on February 18, 2007, 11:47:14 AM
Quote
Originally posted by Krusty
Knegel, you're saying you need 100% more lift to bank 45 degrees. You don't. You can bank 45 degrees without flaps and not fall from the sky.


Hi,

of course yopu dont need 100% more lift to bank your plane, but to keep altitude.

At higher speed it might be that the fuselage provide extra lift (siderudder oposide to the bank direction), but in gegeral you need to pull the stick if the plane got banked by 45° to increase the lift, otherwise the plane will sink down rather fast.

If a plane get banked to 90° the wing related upward lift get minimized to 0 %, with 45° it 50% , in level flight 100% point upward.

You can try it in AH, fly a plane, bank it to 45° and dont pull the stick.


Greetings,

Knegel
Title: Re: Spit 16
Post by: WpnX on February 18, 2007, 04:14:14 PM
Quote
Originally posted by loony1
something needs to be done about the spit 16 it is totally over modeled

...., so i don't need any flames on my flying skills. ...


Sounds like you need to work on your flying skills:)
Title: Spit 16
Post by: dtango on February 19, 2007, 06:16:45 PM
Here are a few points that I thought were worth discussing in this thread that I hope illuminates the subject a bit more:

Don't assume that in sustained maneuvering between dissimilar aircraft that the bogey is bleeding energy in a turn even if the bogey is turning tighter than you.  This catches some people by surprise.  Sustained turn performance is primarily determined by the specific energy (Ps) of an aircraft.  Specific energy (Ps) is fundamentally an aircraft's ratio of excess power to it's weight which varies with lift and velocity.   In a sustained turn the plane with the higher relative excess-power to weight ratio will out-turn the other aircraft.

Here's an Energy-Maneuverability chart Badboy posted in another thread (you can find that thread here: http://forums.hitechcreations.com/forums/showthread.php?threadid=194195&referrerid=3699)  that displays some relative Ps data between two aircraft (NOTE: the chart is based on a previous AH FM version but it serves to illustrate the point).

(http://brauncomustangs.org/upload/Sust7b.jpg)

We have an F6F-5 compared to a Ki-84 in the chart.  Both planes are similar in terms of instantaneous turn performance.  There's a difference in sustained turn performance however.  The Ps=0 curve represents the envelope where excess power is equal to zero.  Essentially this is where thrust exactly offsets the total drag of the aircraft produced in a turn.  At the Ps=0 envelope a plane could sustain this turn without losing or gaining any energy.  Above this curve, in a sustained turn the aircraft would bleed E.  Below this curve, the aircraft would gain E in a turn.

Let's assume both aircraft are in a sustained turn with each other at 200 mph with no energy bleed.  You can see that the Ki-84 (point A) is turning both tighter (20 dps, 3.3 g's) and at a smaller radius (850 ft) vs. that of the F6F-5 (point B - 18 dps, 3 g's, 950 ft)….and the Ki-84 is able to do this WITHOUT bleeding any energy!  

I think this type of relative difference in specific energy is one reason of why people are amazed by planes like the Spit XVI.  They expect the other plane (Spit XVI, N1K2-J, you name the plane, etc.) to be bleeding E in a turn when in fact it might be gaining angles on them without even losing any energy at all.  Planes with greater relative excess-power accomplish this because they have greater horsepower/thrust available which offsets the drag in a turn more than another aircraft.  Nothing magical about this.

A plane that is turning at a higher rate and smaller turn radius does not guarantee you an angles advantage.  This is yet another source of  the "how did they do that???!!!" exclamation.  How can my plane that is turning faster and at a smaller radius not win a turn fight?  Here's an example:

(http://brauncomustangs.org/upload/n2n-speed-turns.jpg)

Plane A and Plane B start abeam each other and let's assume that plane A is known as the "better turning plane" relative to Plane B.  Plane A has a higher velocity, better rate of turn and smaller turn radius vs. Plane B.  I've overlaid in light red and blue the turn radius' of both planes to demonstrate that there is a difference in turn circles.  At time 1 they turn into each other.  At time 2 Plane A reverses the turn to attempt a lead turn because of the angular advantage it has gained thinking "I'm the better turning plane!" while Plane B responds in kind in the classic nose-to-nose turn contest.  But Plane B even though it has a larger turn radius and slower turn rate compared to Plane A somehow ends up with angles on Plane A instead at time 4.  How did that happen?  In this situation the relative difference in speeds with Plane B being slower is the deciding factor, not the plane with the better turn radius or the turn rate.

This is one way "better turning planes" are defeated by planes with poorer turn performance and I believe another one of those things that surprises the heck out of people who don't see it coming.

I have a few more things to post but I'll save them for later when I can put them together.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Benny Moore on February 19, 2007, 07:07:31 PM
And that is exactly why American ships do so much more poorly in the game than their real counterparts; the real fighters had much more horsepower to call upon with no weight increase.  Bring on the real ratings, I say!
Title: Spit 16
Post by: Knegel on February 20, 2007, 01:23:09 AM
Hi,

i hope noone mix up excess-power with engine power!!

Excess power in a sustained turn is "thrust power" minus "drag power".


In the example  above plane B dont outturn plane A, what happen is that plane B simply let overshoot plane A.

The pilot in plane A must be a absolut rooki to do the shown manouver.

With two normal skilled pilots plane B never wil outmanouver plane A in a close combat, cause plane A always keep enough enegry to disengage upward in a loop to find himself on the tail of the oponent, while the already slower A cant follow this loop.

Benny, the US planes dont had much more power in real life, the US planes in most cases was rather underpowered, but thats not a disadvantage!!

The late P38J(and L) for example had 2 x 1600HP, on WEP but only a initial climb of 3750ft/min with this setting.

In real life weight/inerta in combination with a rather low drag + a high power engine was more worth than a light nimble but sow plane.

Nothing turned to be more important that the ability to disengage in a smooth dive, to be able to follow other diving planes and to have the initial advantage of a very good upzoom due to a high inertia.

Unfortuately the inertia/weight and weight/drag relation get undervalues in AH, or better sayed, the wingload and powerload factor get overvalued, specialy at high speed. As result planes like the A6M5 and HurriII can follow the dive of a P51 or FW190 rather good and even with 2k distance and a good speedadvanatge this nimble planes will follow the upzoom(due to a incredible lift without the related e-bleed) to get into gunrange again(what is often deadly in AH).

The US planes, same like the FW190, simply wasnt slowspeed turnfighters, they was made to make B&Z war.  The pilots in disadvantage easily could disengage vs the better turning planes, while the better turning planes couldnt, if they was in disadvantage.
As result in real life the faster and higher climbing plane was the better plane to let the pilot survive(if the pilot did know to use the advantage).

Greetings,

Knegel
Title: Spit 16
Post by: Benny Moore on February 20, 2007, 07:37:44 AM
Quote
Originally posted by Knegel
Benny, the US planes dont had much more power in real life, the US planes in most cases was rather underpowered, but thats not a disadvantage!!

The late P38J(and L) for example had 2 x 1600HP, on WEP but only a initial climb of 3750ft/min with this setting.


Nope, that's not at all true.  The P-38L had two Allison V-1710F-30s, each one of which could put out 2,000 hp, giving it a climb rate of nearly 5,000 feet per minute.  Usually they were rated for about 1850 hp. each.  I'm not exactly sure about the horsepower values for the P-47 and P-51, but I do know that their manifold pressures were a lot higher than in game (and that's what determines the horsepower.  P-51D was usually at least 72" Hg. MAP (as opposed to 67" in Aces High II), and the P-47D usually ran about 70" Hg. MAP (as opposed to 64" in the game).

The rest of your claim is fairly true.  However, the early FW-190 was considerably better in a dogfight in reality than it is in the game.  The British captured one and tested it extensively.  The result was that they determined that the early FW-190A was more maneveuverable than the Spitfire Mark V in every way except for turning circle.  That means it out-climbed, out-accelerated, and out-rolled the Spitfire, as well as being faster and having superior dive.  The FW-190 pilot should not be afraid to dogfight Spitfires (until later FW-190s when the power to weight ratio went down).
Title: Spit 16
Post by: dtango on February 24, 2007, 03:59:02 PM
I wanted to help clarify a few things for folks that have been reading this thread specifically as they relate to turn radius.

Some folks are familiar with the following aircraft turn radius equation:

(http://brauncomustangs.org/images/eq08.gif)

This is worth exploring a little.  If a smaller turn radius is an important factor in dogfights what are the ways to minimize turn radius?  Looking at the equation an obvious answer is reduce velocity.  The slower you go the smaller the turn radius right?  Here's another EM chart posted by Badboy (older AH FM but illustrates the point):

(http://www.badz.pwp.blueyonder.co.uk/images/Corner.jpg)

In the diagram why then does the turn radius get larger vs. smaller the slower below corner velocity each plane gets?  

(http://brauncomustangs.org/images/eq08-m2.gif)

The answer is that g's / bank-angle of the aircraft also changes with velocity at as well.  Infact the slower below corner velocity you go the lower the bank-angle achievable therefore the larger the turn radius.  So what is going on here?

(http://brauncomustangs.org/images/TH25G5.jpg)

Basically in a level turn there is a vertical and horizontal component to lift since the plane is banked at an angle to the horizon.  The vertical component still supports the weight. The horizontal lift is what produces the angular acceleration that causes the flight path to curve.  The horizontal lift is opposed by centrifugal (g-force) force due to the turn.  Fundamentally in a turn the aircraft must produce more lift than in level flight due to the additional g-force acting on the plane. The minimun required lift in a turn must equal both the weight and the g-force on the aircraft.  Infact the higher the bank angle, the higher the g-load which means the more lift needed.

(http://www.dfrc.nasa.gov/Education/OnlineEd/Intro2Flight/Images/Wut/WUT7lit.JPG)

(http://www.dfrc.nasa.gov/Education/OnlineEd/Intro2Flight/Images/Wut/WUT8lit.JPG)

So how do we increase lift?  By increasing the angle of attack (lift coefficient - Cl) and/or increasing airspeed since lift is a function of both of these variables.  At lower airspeeds to produce an equivalent amount of lift equal to that at a higher velocity we must increase Cl.  Of course there is a maximum angle of attack (Clmax) for an aircraft and exceeding Clmax results in a stall.  Therefore the envenlope of maximum lift producible by an airplane is at Clmax at that given velocity.  This is referred to as the lift limit which is the left-hand side of the EM plots.

Knowing this envelope also tells us the maximum bank-angle / g-force a plane can support for a given velocity at Clmax.  So we can see how bank-angle / g-force of a plane is limited by the amount of lift an aircraft can produce.  If we fix angle of attack at Clmax then we see that lift varies in proportion with velocity (velocity squared to be exact), therefore the slower you go (below corner velocity) the lower the maximum lift obtainable, the lower the bank angle supported, the greater the turn radius.

Which bring us to the issue of the impact of flaps on turn performance.  Flaps increase lift by either changing the camber of the wing, increasing surface area, or both.  Changing the camber of the wing increases the Clmax of the aircraft.  So what happens when we increase the maximum lift producible by the wing?  Here's yet another EM chart from Badboy that illustrates (note: again older AH FM but it illustrates the point):

(http://www.badz.pwp.blueyonder.co.uk/images/P-38flaps.jpg)

Notice the 1-g stall speeds of the P-38 without flaps and at 5 notches of flaps and how it's much lower with 5 notches vs. not.  Also notice the lift-limit of the P-38 with and without flaps.  With 5 notches we can go slower and yet produce the same amount of lift needed to support the g-load / bank-angle at a higher speed without flaps.  Therefore the we can achieve a smaller turn radius, and also a higher turn rate (at least momentarily) compared to that of the P-38 without flaps.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Squire on February 24, 2007, 07:07:50 PM
The P-38L did not have a wartime rating of 2000hp for its engines, not a typical example anyways!

No reliable source gives them more than 1725 hp at max WEP (which is pretty damn good), for a typical wartime fighter, which was beyond the 1600 hp rating they were actually "advertised as" by Lockheed and Allison, and were the "official" ratings.

I could see asking for the 1725hp rating in the game for the L (@70" Hg) beyond that is getting into pretty iffy territory for a wartime, operational example, of that fighter.

The trouble with many posters, is that you all want the absolute best example of any given fighter, while expecting the "average" ratings for your opposition. Almost ALL the WW2 fighters had examples of tweaked or higher hp models, from any # of causes (fuels, over boosted engines, ect), but its not practical to expect HTC to chase these rarer, souped up versions.

The RAF, USAAF, LW, Soviets, all ran fighters at higher ratings sometimes, but if you do it for one...then you have to do it for all, then it becomes an endless game to chase down the absolute highest examples irregardless of how many really saw action (and the fan-boys dont really care), with the usual endless debates that follow...

They model the average, rated hp's which is really the only sane thing to do. Its "Aces High" not "Reno Air Races High".
Title: Spit 16
Post by: Widewing on February 24, 2007, 08:01:03 PM
Quote
Originally posted by Squire
The P-38L did not have a wartime rating of 2000hp for its engines, not a typical example anyways!

No reliable source gives them more than 1725 hp at max WEP (which is pretty damn good), for a typical wartime fighter, which was beyond the 1600 hp rating they were actually "advertised as" by Lockheed and Allison, and were the "official" ratings.


The 2,000 hp rating comes from data related to the use of 150 octane fuel by 8th AF Fighter Command.

(http://www.wwiiaircraftperformance.org/150grade/engcleared-matcom.jpg)

Few P-38s were operating with the 8th AF when 150 octane came into general use, and it was not used by the 9th AF or any other unit outside of the ETO.

My regards,

Widewing
Title: Spit 16
Post by: Squire on February 24, 2007, 08:04:05 PM
Thats what I figured, I knew under some circumstances they got close to the 2000hp mark, but that wasnt typical for a wartime example of a P-38L.

Like you say, 8th AF didnt use them. P-51 and P-47 did get the fuel though. Even at that, would you have a "typical" P-51 or P-47 with 150 octane? hardly fair unless you go and boost up all the other fighters too, from all the other countries, which was my point.
Title: Spit 16
Post by: Benny Moore on February 24, 2007, 08:18:00 PM
Quote
Originally posted by Squire
[...] the 1600 hp rating they were actually "advertised as" by Lockheed and Allison, and were the "official" ratings.


That's not quite right.  Allison always maintained that they were capable of far more than 1,600 hp., but the U.S.A.A.F. wanted to save wear and tear on the engines.  They never did update the Pilots Manual with the new ratings, but Allison did send their people into the field to show the ground crews how to use the higher ratings.  1725 hp. was obtained from 64" Hg. MAP, but at least 66" was officially approved by the U.S.A.A.F. (not that it stopped many from using more).  Sixty six inches yielded about 1780 hp., using calculations which are not quite precise.
Title: Spit 16
Post by: dtango on February 24, 2007, 08:21:50 PM
Quote
Originally posted by Squire
Thats what I figured, I knew under some circumstances they got close to the 2000hp mark, but that wasnt typical for a wartime example of a P-38L.

Like you say, 8th AF didnt use them. P-51 and P-47 did get the fuel though. Even at that, would you have a "typical" P-51 or P-47 with 150 octane? hardly fair unless you go and boost up all the other fighters too, from all the other countries, which was my point.


Well, the 109K-4 we have is the 1.98 ata version.  So if we've used performance data for the higher HP output for the K-4 why don't we use the performance numbers for the higher rated P-51's and P-47's?

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Benny Moore on February 24, 2007, 08:23:33 PM
It seems there's still debate on that point.  Even the Me-109 fantatics can't agree on which version we have.
Title: Spit 16
Post by: dtango on February 24, 2007, 09:02:57 PM
Oh is that so?  I thought that was answered here:

http://forums.hitechcreations.com/forums/showthread.php?threadid=194384&referrerid=3699

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Squire on February 24, 2007, 09:57:20 PM
Fair enough re: the P-38L. I was only generalising.

Re: The 109K-4, I have no idea what specs they are using. It seems to match the historic speeds and climb from what I can tell. Post different if you have something.

How about a +25 lb (1850hp) Spit XVI from RAF 2nd TAF, which they did use in the war? I can hear the screams from the MA now...

Like I said, there is no end to it once you demand the "bestest" ratings from all these fighters, its a pandoras box. The best method imho, is using more average wartime ratings and keeping the "X-fighter" factor out of it.
Title: Spit 16
Post by: Benny Moore on February 24, 2007, 10:38:40 PM
Well, when you use the "official" ratings for all fighters, the American ships tend to suffer.  Firstly, the higher the ratings are for all fighters, the better off the American airplanes are.  Secondly, American ships often used higher than official ratings, while other countries sometimes used lower than official ratings.

I skimmed that thread, Dtango, and I didn't see any definite answer.  I still have no idea what the Aces High II Me-109K is rated at.
Title: Spit 16
Post by: dtango on February 24, 2007, 11:18:15 PM
Quote
Originally posted by Squire
Re: The 109K-4, I have no idea what specs they are using. It seems to match the historic speeds and climb from what I can tell. Post different if you have something.

How about a +25 lb (1850hp) Spit XVI from RAF 2nd TAF, which they did use in the war? I can hear the screams from the MA now...

Like I said, there is no end to it once you demand the "bestest" ratings from all these fighters, its a pandoras box. The best method imho, is using more average wartime ratings and keeping the "X-fighter" factor out of it.


So why does the K-4 get the benefit of the use of C3 fuel + MW50 but the allied planes don't get to use 150 octane fuel?  We have performance stats for aircraft using 150 octane fuel.  On top of that C3 fuel was hard to come by compared to B4 fuel.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Benny Moore on February 25, 2007, 12:21:33 AM
That is a most excellent point.  At the very least, we could get 66 inches for the P-38, which was not only officially approved but also did not need any special fuel to run.  It was quite possible to run at that pressure using ordinary 100/130 fuel.
Title: Spit 16
Post by: 1K3 on February 25, 2007, 12:57:05 AM
Quote
Originally posted by dtango
So why does the K-4 get the benefit of the use of C3 fuel + MW50 but the allied planes don't get to use 150 octane fuel?  We have performance stats for aircraft using 150 octane fuel.  On top of that C3 fuel was hard to come by compared to B4 fuel.

Tango, XO
412th FS Braunco Mustangs


NOTE:  Fair Play

You see if Allies get their way with having 150,000 octane fuel and Axis with just  vegetable oil, no one will ever play this game

You want your fantasy planes with racing fuel?  Go fly in Il-2/Pacific fighters:aok

Every Luftwaffe, allied, and even Japanese planes use racing fuel there.
Title: Spit 16
Post by: Benny Moore on February 25, 2007, 01:35:30 AM
By your tone I gather that you disapprove of using higher than the lowest official boost for any given model.  So I suppose it's good with you if the Me-109K is given its standard rating of 1.8 atmospheres instead of the 1.98 which we apparently have?  1.8 ata is to the Me-109K what 60" is to the P-38L, and 1.98 ata is to the Me-109K what 66" or 75" is to the P-38L.  Right now we have a high end boost for the Me-109K but a low end boost for the P-38 (and P-51, and P-47, et cetera).  Surely you don't claim that's fair play?
Title: Spit 16
Post by: Neil Stirling on February 25, 2007, 09:47:13 AM
dtango, very interesting chart you have there. Some questions if I may?

Is there a reference that I can quote to get a copy?

Is there a date with the document?

Is it flight tested data? As it looks very much like this:-

http://kurfurst.allaboutwarfare.com/Performance_tests/109G14_May44trials/109G14_GLCE-may44_trials.html

BTW thank you very much for posting it.

Neil.
Title: Spit 16
Post by: dtango on February 25, 2007, 03:27:20 PM
Quote
Originally posted by Neil Stirling
dtango, very interesting chart you have there. Some questions if I may?

Is there a reference that I can quote to get a copy?

Is there a date with the document?

Is it flight tested data? As it looks very much like this:-

http://kurfurst.allaboutwarfare.com/Performance_tests/109G14_May44trials/109G14_GLCE-may44_trials.html

BTW thank you very much for posting it.

Neil.


Neil:

I have no reference or date but I'll check with my source.  Just have the single pic.  Also we don't know if this is flight tested data or not.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: dtango on February 25, 2007, 03:41:26 PM
For the record, I'm not on any "damned fool crusade" (as Obi Wan Kenobi would say!) to get the higher performance numbers for the allied aircraft.  It may be a healthy discussion but at the end of the day HTC get's to make the call regarding what they think is in the best interest of Aces High.

Of course I wouldn't mind if something like perked 150 fuel performance or even a perked P-51H became available :D.  But that's just making known my wish list vs. trying to demand HTC to make it so.

Tango, XO
412th FS Braunco Mustangs
Title: Zeke
Post by: aerosaber on February 25, 2007, 04:08:49 PM
Never seen a a spit turn inside my M2 or 5. May have been extending on you.
Title: Spit 16
Post by: Neil Stirling on February 26, 2007, 10:01:14 AM
Thanks dtango.

Neil.
Title: Spit 16
Post by: Knegel on February 27, 2007, 12:41:16 AM
Hi,

if the 109K4 is a 1.98ata version(C3 + MW50) it should outperform the La7, and Spit16 by easy!! Since is dont do this, i guess its the 1.98ata (no MW50) version, which actually have similar results like the 1.8ata (B4 + MW50) version.


Greetings,

Knegel
Title: Spit 16
Post by: Bronk on February 27, 2007, 10:36:19 AM
Quote
Originally posted by Knegel
Hi,

if the 109K4 is a 1.98ata version(C3 + MW50) it should outperform the La7, and Spit16 by easy!! Since is dont do this, i guess its the 1.98ata (no MW50) version, which actually have similar results like the 1.8ata (B4 + MW50) version.


Greetings,

Knegel


Alt is the determining factor here.

At low alts LA and XVI more than a match. Move it up to med to high alt watch the  109 K4 shine.

Bronk
Title: Spit 16
Post by: Benny Moore on February 27, 2007, 12:27:41 PM
Quote
Originally posted by Knegel
if the 109K4 is a 1.98ata version(C3 + MW50) it should outperform the La7, and Spit16 by easy!! Since is dont do this, i guess its the 1.98ata (no MW50) version, which actually have similar results like the 1.8ata (B4 + MW50) version


Even if were the case that the current, unperked Me-109K is 1.98 but without the nitrous oxide boost, it is still more powerful than the standard 1.8 ata Me-109K.  You people claiming that the U.S. and British ships should only have their "standard" (mid-war) ratings somehow have no problem with the Me-109 having a higher than standard rating.  This is especially troubling because the U.S. and British fighters (as well as the FW-190) used their higher ratings much, much more than the Me-109.

Fair's fair.  If the Me-109K gets a higher than standard rating, then so should the other ships.  If the Me-109K gets the highest rating used in combat, so should the other fighters.  And if one fighter's higher rating is perked, then the historical equivalent for the other airplanes should be as well.

P-38L at 60" = Me-109K at 1.8 ata
P-38L at 66" = Me-109K at 1.98 ata
P-38L at 75" = Me-109K at 1.98 ata plus nitrous oxide

... Or something like that.  The point is that the first pair were the original pressures, and the other ones came later.  It's hardly fair to use the original pressure for the P-38 but a later one for the Me-109, especially since the higher ratings saw much more use for the P-38 than for the Me-109.

What gets to me are the people who think, "The 1.98 ata Me-109 should not be perked, but a 66" P-38L should be."  The 66" rating for the P-38L was not only extensively used, but was official.  The 1.98 ata rating for the 109, on the other hand, was only used on a handful of ships.
Title: Spit 16
Post by: Kweassa on February 27, 2007, 01:36:16 PM
Quote
if the 109K4 is a 1.98ata version(C3 + MW50) it should outperform the La7, and Spit16 by easy!! Since is dont do this, i guess its the 1.98ata (no MW50) version, which actually have similar results like the 1.8ata (B4 + MW50) version.


 Just what standard are you using when you state "one outperforms the other" here? Our Bf109K-4 already outperforms both the Spit16 and the La-7 in many ways.

 Deck-alt speed issues may be the source of skepticism as there are a variety of reports that rate the speed of the K-4 w/C3+MW50 as being considerably faster than as portrayed in Aces High, but the maximum speed of 452mph is a clear indicator in which engine/fuel configuration our K-4 uses, not to mention there has been a consensus in existance for as long as I can remember, that deduced the identity of our G-10/K-4 as being equipped with a DB605DCM.



Quote
P-38L at 75" = Me-109K at 1.98 ata plus nitrous oxide


 There's no such thing as a "Me109K at 1.98ata plus nitrous oxide". Nor is the boost system equipped on the 109s and 190s anything 'special'. The methanol-water injection system is a standard, mandatory piece of equipment that is standardized and equipped on all 109s after the G-14.



Quote
What gets to me are the people who think, "The 1.98 ata Me-109 should not be perked, but a 66" P-38L should be." The 66" rating for the P-38L was not only extensively used, but was official. The 1.98 ata rating for the 109, on the other hand, was only used on a handful of ships.


 The 66" rating was never "cleared", nor was it in anyway "official".

 The circumstantial evidence concerning it's extensive use has a somewhat broad basis, and assumptions that the ("few remaining", if I may add) P-38s in the ETO in late 1944 are clearly very likely to have been using higher boost ratings. However, as Bodie himself states;

Quote
But, meantime get this single fact: Allison Engineering qualified the F-30 engine WER at 1,725 bhp at 3200 rpm. However, the USAAF NEVER authorized that rating, with ATSC preferring to stick with a 3000 rpm limitation. These engines were in Lockheed P-38L, F-5G and P-38M airplanes. Aircraft installation, maintenance, rigging, supercharger performance, propeller performance, etc. all affected individulal engine and airplane performance. And, as certain pilots, including the great Col. Cass Hough who shared command with Col. (later B/Gen.) Ben Kelsey, would have been glad to tell you, if you needed more in combat situations, you did whatever was necessary to escape being defeated.


 The consensus of many would-be researchers seems to be that the above passage is trying to say the 8thAF were 'illegally' using the unsanctioned boost pressures on their planes as a field mod. Bodie, ofcourse, won't go as far as to clearly verify the fieldsmen were defying the orders from the top.

 On the other hand, both the DB605DBM and DB605DCM configurations on the Bf109K-4 were in every sense a truly "official" configuration of the plane which was cleared for use in standard squadron service. The rarity of the DB605DCM configuration comes from the fact that the C3 grade fuel was largely required for the Fw190s, which was absolutely necessary for flight, unlike the Me109s which can use standard 87octane B4 grade fuel as well. They were losing the war, the fuel supply wasn't enought. The C3 went to the 190Ds, not to the most of the K-4s.

 There is a very, very excellent discussion concerning the existance of these "late P-38Ls" in the IL2 forums, with the participants of both sides coming up with equally interesting and convincing evidence:

P-38L 'late' - the new fantasy plane? (http://forums.ubi.com/eve/forums/a/tpc/f/23110283/m/3351093733/p/1)


 ...


 HTC sticks to the principle of what we fans call the "official standard". HT has never elaborated just what this is, nor acknowledged the actual existance of such a policy,  but over the years us AH gamers have come to believe that this principle is roughly something like;

1. The planes are modelled according to the most representative of official data set, inclduing official flight tests of sanctioned/standard plane configurations and pilots manuals.

2. When a non-primary, or secondary evidence states a different performance figure coming from a 1) controversial source, 2) individual pilots anecdote, 3) a plane with modified and arbitrary configurations that was never officially sanctioned, the differences are NOT reconciled. There is no 'compromise' in figures. Only the official data set is used, and the rest is dropped.

3. When a certain plane has a multiple set of differing 'official figures', the one most represantative of its major career as a fighter aircraft may be used. For instance if a certain plane is introduced in early 1944. and then its standard performance was increased only in the last few months of the war, then the performance figures during its introduction would be preferred over the figures during the last months of the war.

4. The reason behind the 'official standard' policy is that dabbling into controversial or unclear, unconfirmed data may start a chain reaction of skeptical performance figures being introduced into the game. When one group of planes starts using dubious, anecdotal figures for their planes, there is no basis to stop other planes from using strange figures as well. The line has to be drawn somewhere.


 The problem is that HTC doesn't necessarily strictly adhere to these principles, which is often a source of confusion. Or sometimes, the plane modelled in AH might have multiple aspects of different configurations that even identifying the exact configuration itself seems to be difficult. A prime example of these two problems would be the Bf109K-4.  In other cases, such as the P-38s, there exists a considerable amount of evidence the P-38s did use higher boosts, and yet there is not a single piece of official document that states the P-38s were ever cleared to use the 66" / 1725hp / 3200rpm configuration. However the case of the P-38 clearly falls under the 3rd perceived rule as mentioned above.

 Personally, I believe the higher boost ratings should be included in the game as a perked option, and such measures should be standardized with all planes (for example our Bf109F-4 using 1.42ata, should be derated to 1.30, and the 1.42ata should be given as a perked option). But this is this, that is that. Benny's argument that the 66"/75" P-38L should be introduced on grounds of 'officiality' is clearly wrong.
Title: Spit 16
Post by: Knegel on February 27, 2007, 02:06:34 PM
Hi,

i think you have a misunderstanding regarding the 109K engine. The DB605DB had the same max power with B4 fuel + MW50 or C3 fuel  without MW50.

The AH 109K4 have a Vmax of roundabout 590km/h(366mph) at sea level, thats what this plane did reach with 1.8ata C3 fuel or 1.8ata B4 + MW50.

And this was the absolut common version of the K4, already the K10 did use this engine! The poweroutput at sea level was 1850PS, 1600PS at 6000m and 1275PS at 6800m.

The K4 with DB605DC(1.9-1.98 ata) was rather seldom and would have had 2000PS at sea level, 1800PS at 4900m but also 1275PS at 6800m, with this power it should outperform the La7 also at sea level. This setup should for sure be perked, simply cause it was rare.

The DB605DC only with C3 fuel  on Start/Not(no MW50) had less power than the DB605DB.

Up to 6000m the K4 simply was one of the best accelerating planes in WWII, it had other disadvantages.  

Greetings,

Knegel
Title: Spit 16
Post by: Bronk on February 27, 2007, 02:21:40 PM
Quote
Originally posted by Knegel


Up to 6000m the K4 simply was one of the best accelerating planes in WWII, it had other disadvantages.  

Greetings,

Knegel


Hmm just like in game. Only a few can out accelerates it .


Bronk

Edit: I think only the Tempest and La7 can out accelerate it.
Title: Spit 16
Post by: TUXC on February 27, 2007, 02:26:13 PM
Wasn't the 109k with 1.98ata capable of 377mph on the deck? (I got that from Kurfurst's 109 webpage). Ours is about 10mph slower that that going by the chart in the hangar in the online game.

I think this is the first time I've seen people complaining about a German fighter performing too well.;)  It's a welcome change, but I hope the 109k gets left as is. It's not like everyone is flyng it in the MA anyways....otherwise it'd already be perked!
Title: Spit 16
Post by: Krusty on February 27, 2007, 02:30:07 PM
Yes... it's only been "recently" that some folks say we have 1.98ata. Up until now nobody has ever argued this, in fact most said the opposite, and begged/pleaded for 1.98ata to be included in the game.

I don't buy that 1.98ata is modeled, currently.
Title: Spit 16
Post by: Bronk on February 27, 2007, 02:30:28 PM
Quote
Originally posted by TUXC
Wasn't the 109k with 1.98ata capable of 377mph on the deck? (I got that from Kurfurst's 109 webpage). Ours is about 10mph slower that that going by the chart in the hangar in the online game.

I think this is the first time I've seen people complaining about a German fighter performing too well.;)  It's a welcome change, but I hope the 109k gets left as is. It's not like everyone is flyng it in the MA anyways....otherwise it'd already be perked!


AHHHHHHHHhahahahhahhhaahaa.
Barbi is teh king (or is that queen )of the cherry picked data.
Take anything by barbi with a huge grain of salt.

Bronk
Title: Spit 16
Post by: Krusty on February 27, 2007, 02:42:38 PM
He would interpret it poorly, with a huge bias, but even Kev's quoted as saying his data is relatively sound.
Title: Spit 16
Post by: F4UDOA on February 27, 2007, 03:26:36 PM
Kweassa,

You make a good point about modeling representitive aircraft instead of the limited or possibly even the test bed aircraft performance that was by far the exception rather than the rule.

AH does a great job putting out the FM that best represents the aircraft that actually fought in combat. Almost any aircraft with fine motor control could be overboosted for a period of time before predetonation or overheating becomes an issue (overheated leads to Pre-detononation). The performance modeled in AH is the performance listed by the corresponding forces that flew them and the manuals that dictated the limits of there use.

The really funny thing is that the only performance stat in AH that people really get stoked about is top speed at sea level which in actual combat was about the last place anyone cared about performance however in the MA it is the single greatest criteria to measure an aircraft by.
Title: Spit 16
Post by: Kweassa on February 27, 2007, 05:09:24 PM
Quote
...however in the MA it is the single greatest criteria to measure an aircraft by.


 Probably the single most defining difference between game combat and actual combat, I believe. Differences in pure maneuverability, or differences in deck speed and such would rarely be of such high importance when assuming a more organized combat where the reactions concerning individual aircraft in a cohesive manner would do far more good than contesting every enemy in a deathlock duel.
Title: Spit 16
Post by: Kev367th on February 27, 2007, 05:35:13 PM
Quote
Originally posted by Krusty
He would interpret it poorly, with a huge bias, but even Kev's quoted as saying his data is relatively sound.


Kurfys data was 'sound' up to the point he shows various docs etc, but no hard proof 1.98ata was ever used on even a single K4.

Me makes a lot of "we can assume", "we can suppose" comments, but nothing to actually back them up.

Even a doc I found shows all the K4 units still using B2 fuel (C3 required for 1.98ata) at the end of March 45.
Only evidence of 1.98ata for 109's was a couple of flights of G-10's using it for 'operational testing' in Jan 45.

Thankfully HT doesn't base FM's on "we can assume", "we can suppose".

Main problem was Kurfys different standards for proof.
We were supposed to accept his assumptions, yet when proof (sqn/line docs) was shown of Spit XIV's converting to 21lbs boost he would say "well thats just one aircraft".
Show the whole squadron converted, "well thats justy one squadron".
Show more than one squadron converted, "well thats just a few squadrons"
You couldn't reason with him.
Title: Spit 16
Post by: Benny Moore on February 27, 2007, 06:45:37 PM
Quote
Originally posted by Kweassa
The 66" rating was never "cleared", nor was it in anyway "official".

Benny's argument that the 66"/75" P-38L should be introduced on grounds of 'officiality' is clearly wrong.


That's not true.  I don't have it, but I have seen the document officially approving 66" for the P-38L.  I believe Widewing will be along shortly to post it.  I've also seen documents approving 72" for the P-51D and 70" for the P-47D.  This is for operational service, not a test aircraft or two.

Quote
Originally posted by F4UDOA
The really funny thing is that the only performance stat in AH that people really get stoked about is top speed at sea level which in actual combat was about the last place anyone cared about performance however in the MA it is the single greatest criteria to measure an aircraft by.


Balogna!  Power doesn't just improve speed, it dramatically affects climbing abilty, acceleration, and turning ability.  In short, it improves your fighter in every way with no drawbacks (except that you're more likely to break your ship up from overstress if you're stupid).  Try sometime reducing power to nine tenths of maximum throttle for the entire duration of a dogfight and see how well you do in any of the fighters we're talking about (P-38, P-51, P-47, FW-190, Me-109).
Title: Spit 16
Post by: MiloMorai on February 27, 2007, 06:46:51 PM
This is in the sig  of a poster over at Ubi

Kurfurst logic: 'cleared' = 'used' for the LW = 'not used' for the Allies; 2 = quite a few ships

He used have, but was removed for some reason,

Kurfurst Motto: The truth, the whole truth and nothing but the truth >> NEVER

Kev, B2 fuel?? B4 fuel should it not be? Me109Ks also used C3 fuel(1.80ata).
Title: Spit 16
Post by: Benny Moore on February 27, 2007, 06:49:58 PM
Don't even get me started on Kurfurst.  I have only one word to say about that individual - serial liar.  All right, that was two words.  Oh, well ...
Title: Spit 16
Post by: Benny Moore on February 27, 2007, 07:01:36 PM
Quote
Originally posted by Kweassa
The 66" rating was never "cleared", nor was it in anyway "official".

Benny's argument that the 66"/75" P-38L should be introduced on grounds of 'officiality' is clearly wrong.


That's not true.  I don't have it, but I have seen the document officially approving 66" for the P-38L.  I believe Widewing will be along shortly to post it.  I've also seen documents approving 72" for the P-51D and 70" for the P-47D.  This is for operational service, not a test aircraft or two.

Quote
Originally posted by Kweassa
There's no such thing as a "Me109K at 1.98ata plus nitrous oxide". Nor is the boost system equipped on the 109s and 190s anything 'special'. The methanol-water injection system is a standard, mandatory piece of equipment that is standardized and equipped on all 109s after the G-14.


Right, I was wrong about the nitrous oxide; a quick search shows it was only used on early 109s.  I meant methanol injection.  But what about Knegel's claims that some Me-109Ks ran at 1.98 ata but did not have methanol injection?

Quote
Originally posted by Kweassa
There is a very, very excellent discussion concerning the existance of these "late P-38Ls" in the IL2 forums, with the participants of both sides coming up with equally interesting and convincing evidence:

P-38L 'late' - the new fantasy plane? (http://forums.ubi.com/eve/forums/a/tpc/f/23110283/m/3351093733/p/1)


That discussion is good - and only good - because of the data posted by Big Kahuna and company.  Kurfurst is a liar, and he was lying then.  I've seen with my own two eyes a document clearing the P-38L for 66" Hg. MAP.  He's also wrong about the horsepower; 1725 hp. comes from a 64" rating, not 66 inches.

Kurfurst was also lying when he slandered Big Kahuna, accusing him entirely without evidence (or provocation) of fabricating those figures - figures which Big Kahuna had clearly stated in previous threads where he got them (Warren Bodie).

By the way, I have to retract some of the statements I made in that "fantasy plane" thread; it was several years ago and I hadn't seen some of the documents I have now.  I mentioned that the P-38L could run at 1725 hp. when using 150 fuel, but it actually could also run it on standard 100/130 quite handily.
Title: Spit 16
Post by: Widewing on February 27, 2007, 07:57:25 PM
Quote
Originally posted by Benny Moore
That's not true.  I don't have it, but I have seen the document officially approving 66" for the P-38L.  I believe Widewing will be along shortly to post it.  I've also seen documents approving 72" for the P-51D and 70" for the P-47D.  This is for operational service, not a test aircraft or two.


From http://www.wwiiaircraftperformance.org:

The 150 octane P-38 test report can be found here. (http://www.wwiiaircraftperformance.org/p-38/p-38-28392.html)

My regards,

Widewing
Title: Spit 16
Post by: Benny Moore on February 27, 2007, 09:17:55 PM
Thanks.  I've also seen a picture of an actual document clearing 66" for operations; do you know where I can find that again?  I was an idiot not to save it at the time.  That 70" test and recommendation is good enough for me, since I already know from a myriad of sources that ratings well above that were used in combat, but some people are not happy unless they see an official document (and even that's not good enough for individuals like Kurfurst).
Title: Spit 16
Post by: dtango on February 27, 2007, 09:56:34 PM
Sorry guys, I had posted a chart earlier that I asked HTC to remove on the 109K4.  It helps to first to get the permission of your source for data for posting before posting it!

At any rate:  most folks have recently quoted kurfurst's messcmt documents for performance on the 109K4.  At worst the AH 109K4 is the 1.98 ata C3 version (without MW50).  At best it's the 1.98 ata  C3+MW50.   The messcmt document that kurfurst's charts come from state that compressibility is not accounted for which means the quoted speeds would be lower than on the charts.  If I recall there's fw190 data out there that has oft been quoted that has the same issue of not being corrected for compressibility drag.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Benny Moore on February 27, 2007, 10:12:17 PM
Kweassa says that all Me-109K's had MW-50.  If that's true, then we have a 1.98 ata Me-109K with MW-50, and therefore should get higher boosts for other airplanes (since, after all, very few Me-109s used 1.98 ata, while lots of other ships used their higher ratings).
Title: Spit 16
Post by: Krusty on February 28, 2007, 12:01:33 AM
Benny... you're assuming a lot.

You're ASSUMING that we have a 1.98 boosted K-4. You're putting too much emphasis on the MW50. It was like water injection on later US rides, quite common.

You can have MW50 on any level of boost, it just helps prevent detonation in the engine.

Having said that, even the 1.8ata K-4 (which we probably have) still has MW50, and always has.
Title: Spit 16
Post by: Knegel on February 28, 2007, 01:45:59 AM
Quote
Originally posted by Benny Moore
Don't even get me started on Kurfurst.  I have only one word to say about that individual - serial liar.  All right, that was two words.  Oh, well ...


Isnt it a "bit" poor to sidekick to someone who isnt here to defend himself, specialy if we see that very similar systems of argumentation like Kurfi use get used??(im not only talking about you Benny!)

The way Kurfi rate the datas of different nations and planes often looks biased and iam sure he dont do a good job for his own preferences, cause often people tend to throw the helve after the hatchet.

Only cause Kurfi did offer documents, they are not bad and the 109K4 DB605DB/ASM datas we have show 590km/h at sea level and a climb of 1500m/min in its peak.

With a "Dünnbrettpropeller" we the K4 is shown a bit faster. Noone need to argue that this speeds could vary up and down, from plane to plane etc, we all know that, but realy, why a so smal, streamlined  and light plane with 1850PS shouldnt be so fast??
The 109F4 with only 1170PS did reach already 529km/h +-6km/h, almost 700PS more should help a lot.  

The more big La7 with same power is faster in AH and the much more big and heavy P51B and D with particular much less power are same fast.  And i wanna see the calculation that determine that a semi-laminar airfoil is able to even out the drag of 5m² wingarea and much more big fuselage and 100-300HP and 1000kg more weight.  :rolleyes:

Just to say, i saw the P51 tests and they are a fact, to say the available K4 datas are "Kurfi propaganda" is where i have a problem.  That the K4 with 1850PS, but also the Spi14 are only as fast as the much more big, much more heavy and less powerfull P51 already is strange and show how advanced the P51 design was regarding speed.

btw, 600km/h @ sea level are still far away from compressibility problems.

Greetings,

Knegel
Title: Spit 16
Post by: Kweassa on February 28, 2007, 03:23:52 AM
Quote
That discussion is good - and only good - because of the data posted by Big Kahuna and company. Kurfurst is a liar, and he was lying then. I've seen with my own two eyes a document clearing the P-38L for 66" Hg. MAP. He's also wrong about the horsepower; 1725 hp. comes from a 64" rating, not 66 inches.


 I've read the entire thread. No documents were presented that actually showed an official approval of the use 66" on the P-38L. The closest thing that was presented was a informal memo of a new engine configuration scheme that offset some of the aircraft manifold ratings to higher levels with the use of better grade fuel, and even in that memo the plane that is mentioned is the P-38J, not the L.  Nor is the info presented by Widewing an approval - it's a flight test data.

 Now, I'm not contending the P-38Ls never used higher boost settings in the latter days of the war. However, I am contending that it was a measure that was never sanctioned officially, used on a few remaining squadrons that actually retained the use of P-38s as all the other squadrons have long since converted to the P-51(Look at the dates on Widewing's flight test). That's exactly what Bodie himself is stating.


Quote
Kurfurst was also lying when he slandered Big Kahuna, accusing him entirely without evidence (or provocation) of fabricating those figures - figures which Big Kahuna had clearly stated in previous threads where he got them (Warren Bodie).


 In a sense of fairness viewed by a 3rd person with no direct interestes to either side, both parties were assuming a lot upon insufficient data. Kurfy is notorious for his biases and aggressive interpretations on data, but he does not conjure anonymous numbers up. He refuses to acknowledge that the numbers of evidence mounting on the use of higher manifold settings on the latter day P-38Ls are substantial, which in my view is clearly problematic.

 However, the same sort of overly enthusiastic interpretation also comes from the proponents of the P-38L themselves. An ironic example would be you yourself here, who is vouching fot Kahuna's interpretation on the subject based on Bodie, and yet you refuse to believe Bodie's own statement on how the 8thAF never officially sanctioned the use of 66" on the P-38L. That's selective reasoning.


Quote
By the way, I have to retract some of the statements I made in that "fantasy plane" thread; it was several years ago and I hadn't seen some of the documents I have now. I mentioned that the P-38L could run at 1725 hp. when using 150 fuel, but it actually could also run it on standard 100/130 quite handily.


 Not according to that thread. Kurfy's not the only one against the "P-38L late". From my point of view, running 1725hp on 100/130 is an assumption at best. It probably could run at that rating, but it didn't.
Title: Spit 16
Post by: Benny Moore on February 28, 2007, 07:35:56 AM
I can only assume that Bodie is not aware of the memorandum which, I repeat, I have seen clearing 66" for operational use.  This is important; at the time of that "fantasy" thread I was relying mostly on the word of Big Kahuna, Gibbage, and a few other associates.  However, in the years since then I have done a lot of research and accumulated a lot of data.  I base my statement on the 66" operational use on an official document I've seen a full scan on.  It's a memorandum from a general authorizing 66" for operational use on the P-38L in Europe.  It's understandable that you disbelieve me until I provide evidence, so I shall search hard for this document.  You might want to check out Vees for Victory; it mentions Allison tests that 130 octane fuel was sufficient to run 66".

You say that Kurfurst refuses to accept the numbers.  That's an understatement.  In the thread, he flatly states that 1600 was the P-38's horsepower and that there was no 1725 hp. P-38.  This is a lie, and he provided no evidence supporting his bold statement.  He also failed to completely to counter the evidence of others.  But that's not the biggest problem.  As I said, Kurfurst accused Big Kahuna and others of fabricating data.  That's pretty big.  Again, he never provided an ounce of evidence to back up his outrageous claims.

Even if there were no evidence to indicate that 1780 or 1725 hp. were used operationally (which is not at all the case), it's still very wrong to state that 1600 was absolutely the maximum horsepower on the P-38.  The implication is that 1600 was the hard and fast limit, that the engines were not capable of putting out more power.  It's one thing to claim that only 1600 saw service (which is wrong it itself), but it's quite audacious to say that 1600 was the maximum power of the P-38 (especially when you already know about higher ratings).

Kurfurst is a liar, and probably always will be.  Don't you believe a word he says; I've seen him say two opposite statements about his precious 109 in two different threads on the same day, depending on the person he was talking to.  As for the mild suggestion that I am acting similarly to Kurfurst - that would be me stating flatly that there was no such thing as an Me-109 running 1.98 ata.  It is a fantasy plane.  Kweassa and Knegel made up those numbers or got them from the internet.  1850 was it's maximum horsepower, and the 2000 horsepower figure is poppycock.  And the 109 never ran on C3 fuel.
Title: Spit 16
Post by: Kev367th on February 28, 2007, 09:20:08 AM
Quote
Originally posted by MiloMorai
This is in the sig  of a poster over at Ubi

Kurfurst logic: 'cleared' = 'used' for the LW = 'not used' for the Allies; 2 = quite a few ships

He used have, but was removed for some reason,

Kurfurst Motto: The truth, the whole truth and nothing but the truth >> NEVER

Kev, B2 fuel?? B4 fuel should it not be? Me109Ks also used C3 fuel(1.80ata).


CC, B4 my bad.

Yes, but they could use C3 or B4.
The only change being if any were converted to 1.98ata they could ONLY use C3 fuel, according to Butch.

That has been one of the arguments against it happening.
With the falling fuel production that they would limit an aircraft to one specific fuel, when previously it could use either.

The only way the LW were able to almost maintain a steady sortie rate from Jan 1945 onwards, was to cut fuel supplies to everything non-essential and divert it to frontline units.

Lets have the XVI at 25lbs boost.
It was used on the LF IXe from May 1944.

The XIV at 21lbs - July 1944.
Title: Spit 16
Post by: Bronk on February 28, 2007, 12:31:57 PM
Quote
Originally posted by Knegel


The more big La7 with same power is faster in AH and the much more big and heavy P51B and D with particular much less power are same fast.  And i wanna see the calculation that determine that a semi-laminar airfoil is able to even out the drag of 5m² wingarea and much more big fuselage and 100-300HP and 1000kg more weight.  :rolleyes:
l


In game on runway full fuel no drop tanks. Using the E6B

La7         7390 lbs    21 min of fuel
109K4     7563 lbs    27 min of fuel
XIV          8574 lbs    26 min of fuel
P51D       10089 lbs  50 min of fft
P51d @ 50% fuel 9363 lbs 26 min of fuel.

So the difference for the 51 vs k4 is down to 816 kilo

Can prop design and aerodynamics compensate for top speeds?

Now using Gonzo's  web calculator. Found here
http://gonzoville.com/ahcharts/index.php


Off wep in game the 51d is faster than the k4 up to 16.5K.
On wep on the deck speed almost identical, after that the 109 is faster at all alts.

Now as far as climb and acceleration the k4 stomps the 51d in both.

So I have no idea how you can say the the 51 is just as fast because its not.

Now the La7 has makes 2000 hp at 2600 rpm at sea lvl. Per this thread http://forums.hitechcreations.com/forums/showthread.php?s=&threadid=198148

Now plug in the la7 and the K4 in gonzo's calc.

On wep the 109 accels almost as fast but out climbs the La7.
Then once to about 5k feet the k4 is faster on wep and really starts to out climb.
At 13k it becomes faster off wep.

The complaint that the k4 is not up to snuff in game is silly.



Bronk
Edit: Whats the HP difference off wep with the d and k4 at low alts?
Title: Spit 16
Post by: TimRas on February 28, 2007, 03:05:36 PM
Quote
Originally posted by dtango
Well, the 109K-4 we have is the 1.98 ata version.


How do you know that ?

E6B data below:

(http://img.photobucket.com/albums/v424/timppa/K4-1.jpg)
Title: Spit 16
Post by: Squire on February 28, 2007, 04:13:06 PM
He's alleging that it flys with the 1.98 ata flight data, at 1.80 ata. At least I beleive thats the accusation.

Im doubtfull myself, as the FMs in AH are modeled with weight, drag, and h.p. inputted, rather than older FMs that had flight data set in alt "bands" with set #s.
Title: Spit 16
Post by: dtango on February 28, 2007, 08:12:42 PM
Accusation?  Wow, I'm not accusing anyone of anything as if something was wrong.

I am saying that the 109K4 we have in AH seems to be pretty darn close to the 1.98 ata performance.

Let's just take the Mtt documents that Kurfurst has posted.  Here's the 1.98 ata C3 + MW50 K4 max speeds:

http://kurfurst.allaboutwarfare.com/Performance_tests/109K_PBLeistungen/files/5026-18_DCSonder_MW_geschw.jpg

Top speed at critical alt we have ~727 kph/ 452 at 21k.  The AH K4 top speed is ~452 mph.

At SL max speed is ~610kph/379mph.  The AH K4 is slower at ~370mph.


Let's take a look at the Mtt documents again for the 1.98 C3 without MW50:
http://kurfurst.allaboutwarfare.com/Performance_tests/109K_PBLeistungen/files/5026-26_DCStart_noMW_geschw.jpg

For the 1.8 ata and 1.98 ata without MW50 the top speed is ~720kph/447mph (vs. the AH K4 at 452mph).

1.8 ata and 1.98 ata SL max speed is ~590kph/366mph.  This is slower than the AH K4 at SL.

So the AH K4 is better than the 1.8 ata and 1.98 ata C3 no MW50 K4.  It matches the 1.98 ata C3 MW50 K4 at crit alt and but is slower than at SL.

Tango, XO
412th FS Braunco Mustangs
Title: turns with a zeke
Post by: weazely on February 28, 2007, 08:42:08 PM
LOL loony it turns with a zeke if 1 of 2 things happen

1.the zeke isnt turning
2.the zeke pilot isnt ther
Title: Spit 16
Post by: dtango on February 28, 2007, 09:05:19 PM
Knegel:

The compressibility of air creates a lot of different issues.  One of the effects is a rise in drag with increasing mach number known as compressibility drag.  It's different than what you are thinking about - e.g. the effects of compression on aircraft control (e.g. buffeting, stiff controls, tuck-under, etc.).

At lower subsonic speeds we treat air as incompressible.  As airspeeds increase you have to account for the drag due to compressibility because of the changes in the pressure distribution.  Here's a graph of the impact of compressibility drag on the XP-51.

(http://brauncomustangs.org/images/cdrag.jpg)

For reference to the compressibility control problems, for the P-51 control and stability issues started to be experienced around mach .75.  You can see from the chart above that compressibility drag increases the drag of the aircraft well below this airspeed.

All aircraft experience this and to accurately assess performance of aircraft you need to factor this in.  The Mtt report on the K4 listed above says that compressibility is not accounted for.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: dtango on February 28, 2007, 09:19:09 PM
One other thing I've noticed people referring to here that I thought I would clarify... weight of the aircraft has little impact on the max level speed of an aircraft.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Benny Moore on February 28, 2007, 10:11:37 PM
I admit I'm grinning right now; Kurfy's own documents are being used for something he would not approve of.  Bwahahaha!

But really ... this does seem to indicate that we have a 1.98 ata Me-109K and therefore it would be logical to include the P-38L at 66" or higher, since (as Mike Williams so kindly proved in the other thread) it saw a lot more service than the 1.98 Me-109K.
Title: Spit 16
Post by: Squire on February 28, 2007, 11:14:42 PM
Poor choice of words, I meant nothing by it.

"Your point was..."

;)

Ok,

...lets see then, we have 447 vs 452 at alt. A difference of 5 mph.

This is easily within the expected error of 1 percentile in any case.

...and its 7 mph slower at S.L.

Your going to have to do better than a measily 5 mph error. I remain skeptical.
Title: Spit 16
Post by: dtango on February 28, 2007, 11:21:02 PM
The same could be said the other way.

at alt 1.98 ata c3 mw50: 452mph vs ah 452 mph (by your calc < 1% ) 0 mph diff.
at SL 1.98 ata c3 mw50 :379 mph vs. 370mph (by your calc < 1%) 9 mph diff.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Squire on February 28, 2007, 11:42:02 PM
Actually, the thing that jumps out at me is the lack of performance boost the 1.98 ata rating seems to give over the 1.8 if the tests are correct.

 Atmospheric conditions, lack or inclusion of wheel well doors, ect, could throw off a flight test by a few mph either way, and I think it is almost impossible to nail down that precisely.

In any case, I dunno if +/- 5 mph (447 vs 452) is worth getting too excited about. I could see it if the K-4 was way over the top in terms of specs, but it doesnt look like it is.

They could model it do 447 tops, and nobody would ever know it unless you told them.
Title: Spit 16
Post by: Bronk on February 28, 2007, 11:49:08 PM
I'd be more interested with acceleration and climb differences.

Top speed might be areo limited requiring much more boost to see bigger gains.


Bronk
Title: Spit 16
Post by: Krusty on February 28, 2007, 11:50:03 PM
But according to even Kurfy's numbers, the top speed wouldn't change. Think of it like the spit1, back before it got 100 octane. Same top speed, just more performance below that point.

I e-mailed Pyro to ask him which version they used when modeling the K-4, no response yet. When I get one I'll post the answer here.

I still don't buy that we have 1.98ata, but I reserve the right to change my opinion if better info comes to light.
Title: Spit 16
Post by: dtango on February 28, 2007, 11:52:23 PM
I don't have any complaints about the K4 being overmodelled in AH at all am certainly not on some crusade to "fix it!!!" :D.   I just thought I would point out to folks the AH K4 is pretty darn close to the 1.98ata c3+mw50 version.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Bronk on February 28, 2007, 11:59:58 PM
Quote
Originally posted by dtango
I don't have any complaints about the K4 being overmodelled in AH at all am certainly not on some crusade to "fix it!!!" :D.   I just thought I would point out to folks the AH K4 is pretty darn close to the 1.98ata c3+mw50 version.

Tango, XO
412th FS Braunco Mustangs


Same here and I agree with you on the boost comparisons.

K4 is great fun to hop in once in a while.

Bronk
Title: Spit 16
Post by: Benny Moore on March 01, 2007, 12:03:25 AM
Quote
Originally posted by Bronk
I'd be more interested with acceleration and climb differences.


Those are my thoughts exactly.  More power means more maneuverability, not just speed.  More power means doing literally everything better, including turn and burn flat turns on the deck.

That's a fair enough way of looking at it, Krusty.  Like you, I am unsure which version we have, so I await the answer from Hitech.
Title: Spit 16
Post by: Bronk on March 01, 2007, 12:16:33 AM
Quote
Originally posted by Benny Moore
Those are my thoughts exactly.  More power means more maneuverability, not just speed.  More power means doing literally everything better, including turn and burn flat turns on the deck.

 


IMHO
To a point I'd say Benny.
To much power with insufficient surface to harness it would make it push . (To steal a nascar term.)


I think it is possible to overpower an airframe.
Torque does strange things to turning ability. Which usually increase a bit  along with HP gains.

109 F4 as a torque  example, slow in a right hand turn.


Bronk
Title: Spit 16
Post by: dtango on March 01, 2007, 12:24:41 AM
Quote
Originally posted by Bronk
I'd be more interested with acceleration and climb differences.

Top speed might be areo limited requiring much more boost to see bigger gains.


Bronk


1.98ata c3+mw50 best ROC: 4920 ft/min (3400 kg?)
1.8ata b4+mw50 best ROC:  4440 ft/min (3400 kg)
1.98ata c3 best ROC: 4320 ft/min (3400 kg?)

AH K4 best ROC:  ~4800 ft/min (3374 kg - assuming AH chart is normally loaded K4).

Assuming the weights are accurate the AH K4 best climb is nearest the 1.98ata c3+mw50 K4.

A correction to the speeds above, I didn't look at the speed diffs for the 1.8ata b4+mw50 version:
SL: ~595kph
alt: ~727kph

Level speeds the AH K4 seems nearest the 1.8ata b4+mw50 in the charts.  

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Bronk on March 01, 2007, 12:34:49 AM
Quote
Originally posted by dtango
1.98ata c3+mw50 best ROC: 4920 ft/min (3400 kg?)
1.8ata b4+mw50 best ROC:  4440 ft/min (3400 kg)
1.98ata c3 best ROC: 4320 ft/min (3400 kg?)

AH K4 best ROC:  ~4800 ft/min (3374 kg - assuming AH chart is normally loaded K4).

Assuming the weights are accurate the AH K4 best climb is nearest the 1.98ata c3+mw50 K4.

A correction to the speeds above, I didn't look at the speed diffs for the 1.8ata b4+mw50 version:
SL: ~595kph
alt: ~727kph

Level speeds the AH K4 seems nearest the 1.8ata b4+mw50 in the charts.  

Tango, XO
412th FS Braunco Mustangs


Lots to ponder on thanks tango.

Bronk
Title: Spit 16
Post by: Charge on March 01, 2007, 04:48:15 AM
"More power means more maneuverability, not just speed. More power means doing literally everything better, including turn and burn flat turns on the deck."

Yes it should. Except for 190A8.;)

"One other thing I've noticed people referring to here that I thought I would clarify... weight of the aircraft has little impact on the max level speed of an aircraft."

Yes. Except for 190A8. ;)

***
"With the falling fuel production that they would limit an aircraft to one specific fuel, when previously it could use either."

As was discussed earlier this is a question of how HTC wants to model a certain a/c. To what it was able to perform provided with certain optimal conditions or what it was historically able to perform in a certain timeframe.

That means that K4 was able to run on 1.98 ATA with C3 fuel (and correct spark plugs), but the fact (?) is that not much C3 was available when K4 was in squadron service.

***
How do you know that the compressibility was not taken into consideration in K4 performace charts? Is it the lack of such statement in the chart or is it specifically mentioned in those chart that it has not been corrected?

***
Do you people know if the intercooler problems which plaqued the P38 were fixed later on? As you know this reduces the power output so that the engine needs to derated to lower boosts to prevent the engine from detonation.

-C+

"Don't even get me started on Kurfurst. I have only one word to say about that individual - serial liar."

Take your "Kurfy bashing" to a board where he can answer you if you are up to it, please. Besides your history on these boards has been so brief that you hardly can state such things about people you hardly know. Of course you are just using it to get acceptance in certain crowds... :p
Title: Spit 16
Post by: Benny Moore on March 01, 2007, 06:13:19 AM
Quote
Originally posted by Charge
Yes it should. Except for 190A8.



That is illogical.  The FW-190A-8 has far more weight than the FW-190A-5.  That is what makes the A-8 worse, not the power.  If only the power were raised and not the weight (as is the case when raising the engine's power rating), it would do everything better, with the aforementioned exceptions of sustained diving at full throttle and instantaneous turn in a certain direction.  It would go faster, climb better, accelerate faster, and turn better.

Quote
Originally posted by Charge
Do you people know if the intercooler problems which plaqued the P38 were fixed later on? As you know this reduces the power output so that the engine needs to derated to lower boosts to prevent the engine from detonation.


Yes, they were fixed in the P-38J.  In fact, it went from having inefficient cooling to having too efficient cooling.  Underheating became a problem at very high altitudes.  Moreover, with 150 grade fuel, running at high manifold pressures (75") was recommended for a minimum of fifteen minutes every flight, regardless of whether or not you needed it.  Apparently, it prevented spark plug fouling or something.

Quote
Originally posted by Charge
your history on these boards has been so brief that you hardly can state such things about people you hardly know. Of course you are just using it to get acceptance in certain crowds...


I was Aerial Target in the linked thread.  I knew Kurfurst quite well.  Big Kahuna (whom Kurfurst repeatedly falsely accused of lying to Oleg Maddox and fabricating data) was the flier who taught me many of the P-38 tricks I know.  As for giving him a "fair fight," I hardly feel that's necessary.  I am not at all slandering him as he was others.  A quick look through a few threads should make that fairly obvious.  If you like, I can provide a list of outright lies of his which, unprovoked, attacked honest individuals.  And then their are outright lies that did not attack anyone, such as his admitting that the Me-109 in Pacific Fighters was overmodelled in climb and later saying that he never said it.
Title: Spit 16
Post by: Charge on March 01, 2007, 06:54:27 AM
"That is illogical. The FW-190A-8 has far more weight than the FW-190A-5. "

Depends on the relative change between the two factors. Strange enough the pilots alledgedly considered the A8 to be the best fighter of FW190A breed.

And the weight does affect its top speed. Although the difference to the mentioned P-51D maybe different because of the wing profile used in these two planes. Maybe the laminar flow wing is less sensitive to profile incidence angle change because of the weight increase.

"Moreover, with 150 grade fuel, running at high manifold pressures (75") was recommended for a minimum of fifteen minutes every flight, regardless of whether or not you needed it."

From MWs docs:

"a.  It is recommended that the Allison V1710-89 and 91 engines be rated at 70.0" Hg. when using 44-1 fuel or its equivalent. Because of the mechanical and maintenance characteristics of the engine and the P-38J installation this rating should be limited to a very short time. Periods between overhaul should be shortened for the engines using this power."

The expression of "short time" is strange. But in all considering the shortened service life before overhaul I find your statement a bit strange. Although it is possible that the engine requires a high pressure run to to keep clean, but 15 minutes? Maybe the restriction was loosened later on?

Im through with Kurfy topic. Not saying he's a saint but not worse than some other people in the other camp, but when he was in these boards back then there where quite heated discussions making not much sense in topic wise.

-C+
Title: Spit 16
Post by: dtango on March 01, 2007, 07:54:13 AM
Charge: RE: compressibility correction...

On the first page of the Mtt K4 document there's a section in German called "macheinfluss:" (mach influence).  On Kurfurst's site they have it translated as:

"Mach effects : Not taken into account in the calculation.
                       Greatest deviation at the Volldruckhöhe with Sondernotleistung, ~5 km/h."

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: dtango on March 01, 2007, 08:01:43 AM
Don't have to the time to post info to make it clear but weight has little impact on the max level speed of an aircraft.  At high airspeeds profile drag dominates and is the primary factor in determining power-required (drag) for the aircraft.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Knegel on March 01, 2007, 09:06:07 AM
Hi dtango,

why do you post the 109K4 datas with the DB605DC, but not the one with DB605DB + MW50??

Actually the 109K4 data sheet with the DB605DB show a better performence than the DB605DC without MW50!!!!!

Datas from the 109K4 DB605DB/ASB sheet:

Vmax sea level: 595km/h!! Like in AH
Vmax 7000m : 725km/h!!  20km/h faster in AH
Best climb : 4400ft/min



Regarding the compressibility:

As we can see on the picture you posted, there are almost no compressibility influences up to 600km/h at sea level(thats less than mach 0,5 at 20°C), thats what i wrote.


Regarding the P51 weight  and K4 speed:

Nowhwere you can read that i wrote the 109K is to slow or to bad in AH, its rather the other way around, some say its to good!!!

The P51D and B in AH fly as fast as the K4 with 100% fuel at SEA LEVEL!!

I took this altitude to compare the speeds, only to minimize the influences by the compressibility(always difficult to estimate) and to show that the 109 with its weight, size and power already must have had a bad propeller etc to be that slow, or the other way around, the La7 and specialy the P51´s must have been better regarding this.

The high altitude speed of the K4 simply seems to be to fast, but since the plane reach the Vmax at 7000-7200m it cant be the DB605DC!!!!

With the DB605DC + MW50 the K4 had its Vmax already in 6000m!!

So if the K4 is to fast in high alt, its something for the bug forum, but nothing to assume the K4 have the 1.98ata engine.

The climb from 200ft + 1min gave me 4500-4600ft/min climb, thats a bit to good, but not realy far off.

Where do you got 4800ft/min from???

btw, in one of my former posts i mixed up the DB605Dc climb(5000ft/min) with the DB605DB climb.

Greetings,

Knegel
Title: Spit 16
Post by: dtango on March 01, 2007, 12:59:27 PM
Knegel:

I assumed the B4+MW50 was going to be slower.  I looked at the chart and realized that according to the chart that was a wrong assumption, so I posted the correction above in my response about the climb rates.  It's up there.  I wasn't trying to selectively hide stuff :).

Regarding 725km/h.  ~725km/h (450 mph) is roughly what the AH K4 is at altitude.  Take a look at the AH speed chart.  It's above 450 mph.

Regarding compressibility - yes at sea level ~595km/h we get mach .48.  But at alt (21k ft) the 725km/h is mach .64.  I was referring to the Mtt report and the quoted speeds there, not your AH tests.  My apologies if that was confusing.  If they aren't factoring compressibility ("mach influence" in the report) then speed listed in the Mtt report at altitude is higher than it would be.

The 4800 ft/min best ROC is from the AH climb chart on their webpage.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Krusty on March 01, 2007, 01:11:53 PM
Quote
Originally posted by dtango
1.98ata c3+mw50 best ROC: 4920 ft/min (3400 kg?)
1.8ata b4+mw50 best ROC:  4440 ft/min (3400 kg)
1.98ata c3 best ROC: 4320 ft/min (3400 kg?)


Really, huh? What alt?

Because even the 109G-14 almost pushes 5000fpm climb, and it's nowhere NEAR 1.98ata. G-14 climb rate is actually BETTER than that of the K-4 between 3k and 10k. Only by a small margin, but this is a draggier airframe with less power climbing better. And it's a heavier frame, too! 7700lbs vs K-4's 7440lbs.

You can't use climb rate to determine boost. That much I'm sure of.
Title: Spit 16
Post by: dtango on March 01, 2007, 01:14:09 PM
Krusty: Look at the highest peaks on the Mtt charts in the climb reports for the K4.  Those are climb rates for a particular boost + fuel + mw50.  I'm just quoting those.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Krusty on March 01, 2007, 01:19:40 PM
http://www.gonzoville.com/ahcharts/index.php?p1=109k4&p2=109g14

^-- what we've got in-game right now. Climb alone doesn't dictate or reflect boost levels used. Unless you're saying the G-14 has 1.98ata, too?? :t


Edit: I'm not picking a fight. I'm just pointing out the climb isn't part of the equation. Too many variables to simply pin it on boost alone.
Title: Spit 16
Post by: Bronk on March 01, 2007, 01:32:43 PM
Quote
Originally posted by Krusty



Edit: I'm not picking a fight. I'm just pointing out the climb isn't part of the equation. Too many variables to simply pin it on boost alone.

He didn't check his previous posts on speeds at alt.:rolleyes:

Bronk
Title: Spit 16
Post by: Ball on March 01, 2007, 01:33:50 PM
why does every thread about the Spitfire turn into 109 rants? ;) :D
Title: Spit 16
Post by: Guppy35 on March 01, 2007, 03:19:59 PM
Quote
Originally posted by Ball
why does every thread about the Spitfire turn into 109 rants? ;) :D


Because the Spitfire apparently always does too much and the 109 always does too little in a flight sim.....regardless as to whether it's true or not :)
Title: Spit 16
Post by: Kev367th on March 01, 2007, 03:29:13 PM
Quote
Originally posted by Guppy35
Because the Spitfire apparently always does too much and the 109 always does too little in a flight sim.....regardless as to whether it's true or not :)


Lol

Also usually wanting the LW birds at the max boost they ever flew at, while restricting the Spits to the min boost they flew at.

Still have the whines about the old Spit Vc ringing in my ears, just imagine a 14 @21lbs and a 16@25lbs.
As they allow LF IXe skins on the XVI it's clear they consider them (rightly) the same aircraft, you could have a 25lbs LF IXe from May 1944 :) .

[edit] To be fair it only appleis to a small minority. They usaully require more and a higher standard of proof for Spit boost levels than what they are prepared to give for the LW birds.
Title: Spit 16
Post by: Benny Moore on March 01, 2007, 03:39:04 PM
Quote
Originally posted by Charge
Depends on the relative change between the two factors. Strange enough the pilots alledgedly considered the A8 to be the best fighter of FW190A breed.


You're missing the point.  If you add power, the airplane will do everything better.  If you add weight, the airplane will do everything worse (except dive).  Any decrease in performance in later Focke-Wulfs is due to weight increases, not power increases.  Quite the opposite, the power offsets the weight.  If you add power without adding weight (which is what raising the rating does), then the airplane will only be better.  Sometime try dogfighting at nine tenths throttle for the whole fight.

Quote
Originally posted by Charge
The expression of "short time" is strange. But in all considering the shortened service life before overhaul I find your statement a bit strange. Although it is possible that the engine requires a high pressure run to to keep clean, but 15 minutes? Maybe the restriction was loosened later on?[/B]


For a P-38J or L, with the drastically improved intercoolers, fifteen minutes is "a short time."  The Allisons themselves were capable of running at 75" for seven hours continuously, according the Vees for Victory, a book about Allison.  Granted, they were not actually in an airplane, and they were fried by the end.  However, it does give us an example of "a long time" from Allison's perspective, from which we can derive that fifteen minutes is a short time.  This is esecially true since pilots were told to run for that time on every flight, whether or not they needed the extra power.
Title: Spit 16
Post by: dtango on March 01, 2007, 10:27:36 PM
Quote
Originally posted by Krusty
http://www.gonzoville.com/ahcharts/index.php?p1=109k4&p2=109g14

^-- what we've got in-game right now. Climb alone doesn't dictate or reflect boost levels used. Unless you're saying the G-14 has 1.98ata, too?? :t


Edit: I'm not picking a fight. I'm just pointing out the climb isn't part of the equation. Too many variables to simply pin it on boost alone.


1st- rate of climb is absolutely a reflection of power available at a particular boost for a particular engine.  ROC = (T-D)*V/W.  T*V in the equation is thrust power available which is a function of engine power.

2nd- why would I be saying the G-14 boost be at 1.98ata?   The G-10 and K-4 have different engines.  If both planes were at the same boost levels in flight, I wouldn't expect that the engines produce the same power at all because they are different engines.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Knegel on March 02, 2007, 02:38:24 AM
Hi  dtango,

Krusty say that the G10 and G14 climb better than the K4 in AH, therefor the K4 cant run on 1.98 ata, but anyway, i still cant reproduce a 4800ft/min climb, all constant climbs i low level made have 4400-4500ft/min as result.

The climb of the 109K for sure is better than the test show, while the speed is rather ok(i did overview your correction, thanks for the hint), but it looks like the climb of the 109G10 and G14 is to good as well.

btw, no tests on Kurfis page seems to be DB605DC + MW50 related!!

At least i would expect a better climb with 200PS more power from sea level to 4900m, not up to 6000m. It seems to me that it realy is the early DB605D + MW50, which had lower rated altitude than the DB605DB and was more similar to the DB605AM.  

The climbrate with a DB605DC + MW50 should decrease MUCH above 4900m altitude, same goes for the speed, but its almost exact the same climb curve like the DB605DB show, but with a less good performence above 5500m.
Also the Vmax in hight, on the DB605D + MW50 sheet isnt higher than that of the DB605DB, only the Vmax at sea level, but as we know from the La7 and other planes, a Vmax different of 10mph from plane to plane, even with the same poweroutput is nothing special(The La7 test i saw vary from 595-616km/h).
I have no doubt that the 109K4 with 2000PS was at least as fast as the La7 at sea level and the climb must have been better than the DB605DB climb up to 4900m.

Imho the currently to good climb of the 109´s is made to overcome the wrong e-bleed formula while turning, used in AH.  The 109´s with their correct climb would be hopeless, same like the P38´s without the flaps would be hopeless. At least i have no idea why the 109K in low level bleed so much more energy than the La7.  
Imho they should adjust the La7, F4U, Temp, 109F, Spit16 and Hurri(and other rather light wingloaded planes) E-bleed behaviour and they should adjust the 109 climbs(maybe other that are wrong??) to the right values.

The static performences, like Vmax, climb etc are not much worth if the E-Bleed dont work like it should.

The default FM´s of "European Airwar" are a good example to display this:
The 109E4 has a Vmax of 550km/h @ sea level and 1000m/min climb, the Spit1a has a Vmax of 470km/h and 800m/min climb.
This static values clearly show a much to good 109E4, but in game the Spit was a absolut even plane, cause like all other rather light wingloaded planes, it simply didnt bleed energy while turning, also not while highspeed turns.

Imho somewhat similar its in AH(not that extreme). Of course the E-bleed at varius speeds and changing speed is not easy to determine in exact numbers, nevertheless the physical law determine the relations.

And i got the impression that the E-Bleed relation often dont fit in AH.
Heavy wingloaded planes(tendency to have a high dragload) like the P38´s and FW190A8, once fast, should keep energy much better than very light wingloaded planes, specialy if this planes have less power as well.

The 109G6 should keep much more energy than the 109F4, but its the other way around.
The SpitIXc should keep more energy that the SpitVb, but its the other way around, etc.
I only know the A6M2 and A6M5 where this relation fit. The more light A6M2 with its bigger wings bleed more energy while speed decreasing turns than the A6M5. The A6M2 also dont have a that good upzoom, but the relation between this two planes work oposide to how it work otherwise in AH.

Heavy planes with relative smal wings and fuselage simply miss the needed surface to slow down as fast as a more light plane with relative big wings.  Although they need a higher AoA to archive the same turn radius than the more light wingloaded(liftloaded) plane, the surface into flight direction still isnt more big than that of the other plane. At highspeed the higher relative inertia and the smaler relatibe zero drag will help to keep the speed up and and if the other plane turn more tight, it should bleed even more energy.

Thats how it work between the Zeros and thats how it should work in all planes. Only if this relation´s fit, its possible to adjust the static performences(climb, Vmax) to a realistic value, without to get a unbalanced gameplay.

How i would like to be able to make a real B&Z in my P47 or FW190A8 or P38, currently this planes only can make hit and run, even vs outdated planes like the 109F4, HurriII or SpitV.


btw, Benny, weight isnt ALWAYS a disadvantage!!! Weight is a storage of energy, when a P38J meet a SpitV with 550km/h in 1000m alt, the P38J keep twice as much energy + twice as much power than the SpitVb and should be able to outzoom it by easy!!!

Wight hinder the deceleration in the same way like it stop the acceleration.

Why the FW190 and P38 have a so slow acceleration but a so extreme deceleration is a miracle for me.

If HT get this right, we can talk about the static performences(i bet then the P38 dont need more than 2x 1600HP).

Greetings

Knegel
Title: Spit 16
Post by: dtango on March 02, 2007, 09:46:28 AM
Knegel:

Hmm, the Mtt document says the data comes from a DB605DC + MW50.  

2ndly if it was an earlier version of the DB605D then the 1st graph wouldn't make any sense at all.  The power output of the earlier model DB605D's have lower max power output vs. the DC+MW50 engine.

DB605D-2 (C3): 1435 PS
DB605DM (C3 + MW50): 1800 PS

Also the D-2 has a lower output and the DM has about the same power output compared to that of the DB605DB+MW50 (1850 PS).

So if the 1st chart is indeed an earlier version DB605D why are the SL speed and climb rate so much better than the graphs showing the DB605DB+MW50?  So the 1st pair of charts is the same plane but with a lower or equal power output vs. 3rd pair of charts but the plane in the 1st pair of charts has a higher SL speed and better climb rate.  That doesn't make sense.

----
As for the AH ROC figures, the AH charts are showing instantaneous rates of climb.  I'm not sure how you are doing your tests but if you're doing them by averaging them (dividing the total alt climbed by the time to climb) that's why they would be different.  Otherwise the AH charts are incorrect or the weight of the 109K4 you are testing is higher than the weight that the AH charts are generated from.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Bronk on March 02, 2007, 10:04:19 AM
Quote
Originally posted by Knegel
Snip


At 5k the 109K4 exceeds 4800 fpm.
Plug it in here and see for yourself.
http://gonzoville.com/ahcharts/index.php


Bronk
Title: Spit 16
Post by: Knegel on March 02, 2007, 01:53:09 PM
Hi dtango,

once again i made a reading mistake, i thought max climb with DB605D and MW50 is 22,5m/sec, while its 25m/sec.

But anyway, 2,5m/sec also could be a normal fluctuation(look to the different 109G tests we have), 22,5m/sec is pretty low for a 1850PS plane with only 3400kg anyway(compare this with the SpitIXc merlin66 tests and Spit14 tests). With much less powerfull engines and powerloads the 109 airframe did show much better relative results.
Open or closed radiators or a different climb speed can cause such differents.  

It could be the DB605DC on base setting 1.98 ata but using 1.8 ata and 1.9.
This would explain the higher rated alt with MW50 and the only a bit better performence down to sea level, but then thats not the 2000PS of the 1,98 ata.
At least the speedcurve in higher alt is the same like the DB605DC o.MW curve with 1.8ata (7000m 720km/h) and a constant speed gain of only 10km/h(6,2mph) with 150-200PS more power is  also rather strange and also could be normal fluctuation.
Also the curve above "MW50 Abschaltung" is strange, when 1,98 ata got used to 6000m, there should be much less power after dissabling MW50 and the high boost, like we see it in the DB605DB chart. With 1.8 ata this would have been less dramatically like show in the picture. The speed and climb gain could be a result rather of more closed radiators than of a power gain. With 1.8 ata + C3 fuel + MW50, the MW50 could get used only as "Ladeluftkühlung", resulting in a little bit more power, but a more cool engine(less radiator flaps needed).

It also could be the "Leistungsmaschine I" where the testers was refering to, which had a speed gain of 12km/h as result.

Would be interesting to see more background to this test(what ata got used, what radiator flap setting etc).

Greetings,

Knegel
Title: Spit 16
Post by: EagleDNY on March 03, 2007, 02:56:09 PM
Quote
Originally posted by Krusty
Yes... it's only been "recently" that some folks say we have 1.98ata. Up until now nobody has ever argued this, in fact most said the opposite, and begged/pleaded for 1.98ata to be included in the game.

I don't buy that 1.98ata is modeled, currently.


It ISN'T - we are definitely running the 1.8 model according to the 109K testing I just did.  Take one up to 24,600ft, level it out, wep on and see the top speed.  429 Mil / 445 WEP - that is a 1.80 model (even if you don't believe the boost guage which only goes UP to 1.80...).
Title: Spit 16
Post by: Benny Moore on March 03, 2007, 02:57:46 PM
So that must mean that it's not got enough drag, then, right?
Title: Spit 16
Post by: dtango on March 03, 2007, 06:39:27 PM
Quote
Originally posted by EagleDNY
It ISN'T - we are definitely running the 1.8 model according to the 109K testing I just did.  Take one up to 24,600ft, level it out, wep on and see the top speed.  429 Mil / 445 WEP - that is a 1.80 model (even if you don't believe the boost guage which only goes UP to 1.80...).


Both the 1.98 C3+MW50 and the 1.8 B4+MW50 are at 720kph/447mph at 24,600 according to the charts so that's not telling you any difference between the two.  You might try testing it at 19.7K (crit alt for the 1.98 C3+MW50) or at 23.3k (crit alt for 1.8 B4+MW50) to check.

Max top speeds at SL & at Alt suggest that the AH K4 is a very similar to the 1.8ata B4+MW50 version as per the Mtt graphs.  That being said 1.98ata C3+MW50 Mtt graphs max top speeds are similar to the 1.8ata B4+MW50 K4: same top speed at alt (~727 kph/ ~450 mph) but differ by about 8-10 mph at SL with the 1.98ata C3+MW50 at 610kph/379mph.

Climb rate is a different question.  Here's the best ROC comparisons:

AH K4: 4800 fpm @ 4000 ft
1.98 C3+MW50: 4920 fpm @ 2600 ft
1.8 B4+MW50: 4440 fpm @ 2600 ft

The AH K4 has a best ROC more similar to that the 1.98 C3+MW50 version.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Widewing on March 03, 2007, 07:33:32 PM
Maximum speed at best altitude for the AH2 Bf 109K-4 flying with 25% fuel is:

453 mph @ 22,000 feet using WEP.

It does 419 mph at that same altitude in MIL power.

My regards,

Widewing
Title: Spit 16
Post by: Knegel on March 04, 2007, 01:35:13 PM
Quote
Originally posted by dtango

The AH K4 has a best ROC more similar to that the 1.98 C3+MW50 version.

Tango, XO
412th FS Braunco Mustangs


Hi,

for now i dont saw enough datas to say that the DB605D + MW50 sheet is made with 1.98ata. Base setting 1.98 ata dont say that 1.98 ata got used(look to the test without MW50).

At least 12km/h more speed at sealevel would be a real poor gain with 150PS more. The testers wrote that the "Leistungsmaschine I" with its more clean surface etc already did gain this speed and probably also had a better climb. Its a strange chance to see that the test show exact the 12km/h more speed, like the "Leistungsmaschine I" should have had.

I realy believe much, but not that the 109K4 with 2000PS was just as fast as the La7 with 1850PS or that the big and heavy P51B with 75"(around 1800HP??) with wingracks reach 611km/h.

Edit: btw, already 1937 the Bf109V13 with  1660PS did reach 611km/h in an official record trial. So please dont come with a to thick airfoil etc. This plane had the squary wings and the tailwing strutting of the E model.
http://www.adlertag.de/mainindex.htm


Greetings,

Knegel
Title: Spit 16
Post by: dtango on March 04, 2007, 06:55:27 PM
Knegel:

I understand where you're coming from.  I thought I would do a quick check regarding Vmax at sea level for the 1.8 B4+MW50 vs. the graph I believe is a 1.98 C3+MW50.

The aircraft total drag coefficient should give us an indication of what power output the different graphs represent at sea level.  Total drag coefficient should be the same (aircraft hasn't changed).

Fixed Values for Calc:
Wing Area: 173 ft^2
Prop Efficiencey: .81
Air Density: .0023 slug/ft^3 (sea level air density)

Here are the variables:
1.8 ata B4+MW50 : 1850 hp, 370 mph
1.98 ata C3+MW50: 2000 hp, 379 mph

If the 1st graph isn't 2000 hp then we should see a difference in total drag coefficient.  Here are the results:


hp pe thp vmax D (lbs) CD
1850 0.81 1498.5 370 1518.7 0.0259
2000 0.81 1620.0 379 1602.9 0.0260


CD for both aircraft is at .026 which tells me that the first graph is an aircraft at 2000hp.

If it was less (say 1800 hp) CD=.023.

Tango, XO
412th FS Braunco Mustangs
Title: Spit 16
Post by: Benny Moore on March 04, 2007, 10:20:20 PM
And that's the Me-109K in Aces High II?  This is so confusing.  I wish Hitech would come and explain just what kind of K we have.
Title: Spit 16
Post by: Knegel on March 05, 2007, 12:24:44 AM
Quote
Originally posted by dtango

CD for both aircraft is at .026 which tells me that the first graph is an aircraft at 2000hp.

If it was less (say 1800 hp) CD=.023.

Tango, XO
412th FS Braunco Mustangs



Hi,

Thats my point, the rated altitude with MW50 is good above that of the DB605DC at 2000PS and the testers talk about a "Leistungsmaschine I" where they did clean the surface and did gain 12km/h as well.

Already the 109V24 got tested with a CD of 0.24-0.3 depending to the surface. This plane dont had closed wiheelcover , retakeable tailwheel and it did miss the round wingtips.

Greetings,

Knegel