Author Topic: Explain this and win the prize!  (Read 24982 times)

Offline Kurfürst

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« Reply #240 on: November 19, 2004, 04:44:31 AM »
Quote
Originally posted by MiloMorai
As if the 109 did not have protrusions, Issy.:rolleyes:  

Bulges for the cowl mgs, bulges for the wheels, numerous other little bulges and scoops, an air intake sticking out from the side of the fuselage, 3 radiators (2 coolant, 1 large oil), ADF loop, a retractable tail wheel that was sometimes locked down, extended tail wheel strut, gondola guns hung from the wings, . . . . . . .


The point is not that the 109 never degraded aerodynamically during it`s development and when getting new stuff installed. The point is that it was later ALWAYS improved again. The Spit didn`t, as being said the ONLY aerodynamic improvement was the retractable tailwheel, that managed to get a few mph extra, and was used only on very few planes...

As for the 109s, it got two major aerodynamic facelift during it`s development, once in 1940 with the 109F, and in 1943 with the 109K. Which would explain you why it turned out that while in 1940 the Spitfire I was as fast with somewhat less HP, in 1944 it was 60 km/h slower with the same HP...

And just some comment on those drag factors... bulges for HMGs, yes, 9 km/h lost, which wouldn`t matter much in air combat, but the plane was now carrying effective MGs, instead of just ballast like the Spit did until 1944 with those .303s. And then in 1944 those HMG bulges gone.. The Spit had nice big bulges for the cannons through it`s service, THANK YOU desingers who designed a thin wing so much unsuited for bigger weapons, THANK YOU weapon developers in Britain who couldn`t came up with a cannon of their own, and forced the designers to put an large French cannon designed for rigid engine mounts and not flexible wings which cause them to jam.
bulges for the wheels, of course they had it, from 1943, the Spitty had them too, from 1941.
"numerous other little bulges and scoops", yeah, sure they existed somewhere if you say it. :D an air intake sticking out from the side of the fuselage
"an air intake sticking out from the side of the fuselage" - that`s the best one Milo, you are actually critisizing a better aerodynamic solution that reduced the drag.. :rofl  Yep, sticking out the air intake was putting it out of the airstream, which meant an undistrupted boundery layer around the fuselage, the same reason the Mustang did the same with it`s radiator (perhaps because it`s designer was also a former Mtt engineer..)

3 radiators, WOW, Milo, getting desperate, huh? :D It ain`t the number of them counting, it`s the shape. The 109`s was sunken into the wings, having some 40mm sticking out in the front, the whole thing heavily profiting from the meredith effect.. On the Spit, it`s at least half a meter, I STILL don`t get who was that idiot who could design such a monstrosity onto a fighter.. literally drag bags they are, and aerodynamic test show they have serious turbulance inside as a bonus. Again the problem is not that.. the problem is it just worser and worser during the development!

ADF loop, yeah. That`s a classic. Huge drag I guess. :D

"a retractable tail wheel that was sometimes locked down," - hmm, yeah. I guess you mean that whereas the 109 had their retractable t/w *sometimes* locked down, the Spit never really had this problem, as it couldn`t retract the tail wheel in the first place. I wonder though what effect it had on the Spit`s tailwheel drag that it wasn`t lockable either.. lots of turbulance there again.

Gondola guns hung from the wings, yep, optional, raising firepower to a level a Spitfire never had, at a horrific loss of  5 mph. Now for comparison tropicalized Spits lost some 10-15 mph, and that was quite common. Their air intakes were on the nose chin, being as big as the oil cooler on the 109, nicely createing a lot of turbulance all the way behind, smarty positioned at the spot they can eat the most dust from the ground, which meant they needed a filter constantly used which added even more drag, and even then it was useless, the Soviets found the Spit IXs so sensible to dust that they only operated them from the well built airstrips of the PVO in the rear areas..

Mitchel put that plane very nicely together in the mid-1930s... very nice clean fuselage, good for it`s time, nice features, nice characteristics.. but from there it was a downhill run, the whole development can be described with two words : ad hoc.
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Offline gripen

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« Reply #241 on: November 19, 2004, 05:42:28 AM »
The subject of this thread is the efficiency factor of the airplanes and how to determine it. I'm not comparing planes here but looking for what ballpark the e factor  really was.

As an example the F2A-3 had tested efficiency factor about 0,77.

If somebody has relevant information, opinion, or what so ever under this topic; please post! Otherwise cut the crap or start a new thread.

gripen

Offline Angus

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« Reply #242 on: November 19, 2004, 06:53:56 AM »
Good Gripen, good.
I have to have a potshot at Izzy though, forgive me please ;)

Firstly:
"The Spit had nice big bulges for the cannons through it`s service, THANK YOU desingers who designed a thin wing so much unsuited for bigger weapons"

So, it would actually have been better in your your opinion to have the wing much thicker?


Secondly:
"As for the 109s, it got two major aerodynamic facelift during it`s development, once in 1940 with the 109F, and in 1943 with the 109K. Which would explain you why it turned out that while in 1940 the Spitfire I was as fast with somewhat less HP, in 1944 it was 60 km/h slower with the same HP... "

Firstly, in 1940 the Spitfire MkI had roughly the same Hp on 87 oct, and somewhat more on 100 oct.
The Spitfire had less power at high alt, where max speeds were obtained.
Once fitted with a rotol 3-blade airscrew it outclimbed the 109 while being heavier, it was however a tad slower.
Once up to 100 oct the Spit I outclimbed and outran the 109E.

In 1944 you had Spit XIV swarming around. I have not seen data of a 109 being 40 mph faster. So please promote this.

Then here:
"THANK YOU weapon developers in Britain who couldn`t came up with a cannon of their own, and forced the designers to put an large French cannon designed for rigid engine mounts and not flexible wings which cause them to jam. "
You may have a problem here, for the Hispanos were very good weapons indeed. I have not stumbled across any tales of horrible jammings yet. Please promote som.
Very good ballistics, good ROF, and high velocity.
In 1941 perhaps the finest aircraft cannon in the world?

Then finally here:
"better aerodynamic solution that reduced the drag..  Yep, sticking out the air intake was putting it out of the airstream, which meant an undistrupted boundery layer around the fuselage, the same reason the Mustang did the same with it`s radiator (perhaps because it`s designer was also a former Mtt engineer..) "

You must have forgotten take your pills....
The radiator needs air to function, it always causes parasite drag.
Put it in the "shade" and you'll need it to be bigger.
Now, the boundary layer around the fuselage is not as important as say on the top of the wings. Do you know what a boundary layer is? A couple of days ago you did not know what a washout is.
You may of course have a problem with the Mustang, for on the same power as a 109 it was faster, with very much more range. Quite some headache for a brownie-trousers bubchen. But so be it, a German had his hand in on the design so it stays as a so-so.
Frankly I'd like to know what the heck is wrong with you. The only explanation I can think off is complete 1930's German religion, or a brownskirt reincarnation.
I mean, pointing at brilliant design features of objects like the 109, 262 etc is very fine. But you seem so obsessed with hatred on anything WW2 allied sided that it is just stunning. Be it tanks, armies, aircraft, campaigns, victories, political figures, the total outcome or whatever. Anything German just must be better.
Can you tell me why?
All ears?


Regards
Angus



p.s. Sorry gripen


:rolleyes:
It was very interesting to carry out the flight trials at Rechlin with the Spitfire and the Hurricane. Both types are very simple to fly compared to our aircraft, and childishly easy to take-off and land. (Werner Mölders)

Offline Crumpp

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« Reply #243 on: November 19, 2004, 07:15:07 AM »
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Well, the problem is you have claimed things which are not true several times in this thread.


Bull Malarky

Your the one who keeps manipulating your data and using wrong figures to produce your results.  You want us to compare a 1/6 wooden model Spitfire to the actual FW-190A8!!

You cherry pick the best performance data for the Spitfire while using the worst data for the FW-190.  Data which even the flight testers admit they are not getting close to the extimated performance of the Horsepower output.  Data where the flight testers cannot get the engine to idle without fouling plugs and the engine simply quits at altitude to the point the test cannot be completed.

Quote
Not the topic of this thread and learn German...


Your the one who needs to check your German.  Here you attack me and in the other Thread ADMIT it does not say polished or filled!!  It says primed and painted.
Obviously your like a small child having a tantrum when shown to be wrong.

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Offline gripen

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« Reply #244 on: November 19, 2004, 07:31:29 AM »
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Originally posted by Crumpp
Your the one who keeps manipulating...


Well, so far you have not posted anything relevant on efficiency factor nor anything which proves that model testing is bad nor  proof for large scale wind tunnel in the Germany...

Why don't you just make your life easier and post relevant data or shut up.

gripen

Offline Crumpp

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« Reply #245 on: November 19, 2004, 07:42:03 AM »
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nor anything which proves that model testing is bad nor proof for large scale wind tunnel in the Germany...


I don't what to post on that Gripen.  Your a smart guy and have access to some aerodynamic information resources.

Why don't you prove it's not true?

I have told you to make a simple phone call to HTC and ask.

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Offline gripen

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« Reply #246 on: November 19, 2004, 07:49:28 AM »
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Originally posted by Crumpp
Why don't you prove it's not true?


Generally if somebody makes a statement, it's up to him/her to prove it true. The others do not need to disprove it.

If you want to continue, stay on topic and post relevant data if you can.

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Offline MiloMorai

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« Reply #247 on: November 19, 2004, 08:02:51 AM »
Sorry gripen but when Barbi goes on another one of his anti-Spit tirades I can't let it pass.

As can be seen in his reply, he is clueless of what he is babbling about in his delirious state.

Offline Crumpp

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« Reply #248 on: November 19, 2004, 10:44:14 AM »
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If you want to continue, stay on topic and post relevant data if you can.


Exactly,

Your data from a 1/6 wooden model of the Spitfire is not relevant.  You cannot make any meaningful direct comparision between data from a wooden model and compare it with data derived from an actual aircraft of a different type.

Now models are useful for determining general characteristics of the same aircraft.  A wooden Spitfire Model is useful for getting a good idea of how an actual Spitfire will perform but not specifics.

You certainly cannot compare a 1/6th scale Wooden Spitfire to a real FW-190.  You can only make very very General comparisions.  Certainly not to the level of accuracy we are discussing.

This whole thread would have been halted from the begining had I know you were throwing up data off a wooden model.  I just assumed you were smarter than that.

Unless you have a drag polar derived from an actual aircraft then you can only make comparisions using general formulas.
If you get this data please let me know.

Crumpp

Offline Kurfürst

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« Reply #249 on: November 19, 2004, 11:56:10 AM »
Quote
Originally posted by Angus
Good Gripen, good.
I have to have a potshot at Izzy though, forgive me please ;)
[/B]


http://www.hitechcreations.com/forums/showthread.php?s=&threadid=136037
« Last Edit: November 19, 2004, 12:01:19 PM by Kurfürst »
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Offline gripen

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« Reply #250 on: November 19, 2004, 12:49:57 PM »
Quote
Originally posted by Crumpp
Exactly, blaah blaah...


I don't see a reason why you post to this thread If you can't bring in relevant data or you can't prove your arguments.

gripen

Offline Crumpp

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« Reply #251 on: November 19, 2004, 02:16:53 PM »
Your data from a 1/6 wooden model of the Spitfire is not relevant. You cannot make any meaningful direct comparision between data from a wooden model and compare it with data derived from an actual aircraft of a different type.


Crumpp

Offline gripen

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« Reply #252 on: November 19, 2004, 02:28:03 PM »
Well, only you are making comparisons in this thread and please point out the reason why the data from the wind tunnel  with a model should not be comparable.

Besides the Fw data is probably determined with the models as well.

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Offline gripen

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« Reply #253 on: November 19, 2004, 04:10:07 PM »
Here is the Cd/Cl^2 chart for the Spiteful. The data comes from the RAE wind tunnel tests with the 1/5,75 model:



This is a particularly interesting case because there was no washout and the resulting e factor is 0,81.

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Offline Crumpp

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« Reply #254 on: November 19, 2004, 05:11:59 PM »
Gripen,


What does this:

http://1000aircraftphotos.com/APS/2918.htm

Have to do with anything?

Nice info but what does it tell us about the FW-190 vs Spitfire drag picture?

Crumpp