Author Topic: Turn rate hierarchy correlation from actual flight tests  (Read 31614 times)

Offline Jabberwock

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #15 on: October 12, 2009, 10:19:20 PM »
Conventional wisdom, both during and after the war, indicates sustained turn performance:

Spitfire>Bf-109>P-47>FW-190

Most, if not all, anecdotal pilot accounts, place the Spitfire as the second best sustained turner in the ETO, surpassed only by the Hurricane.

You, Gaston, are trying to imitate that :

P-47>Fw-190>Spitfire>Bf 109

Leaves me doing this:  :confused:

Offline Gaston

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #16 on: October 14, 2009, 03:11:31 PM »

  No, the medium-low speed (sustained) turn hierarchy goes something like like this, the A6M5 being at the top:

   Spitfire Mk VIII/IX(+25 lbs)> FW-190A-8 wood prop> Me-109G-14 with MW-50> FW-190A-5> Spitfire Mk V OR P-47D Razorback paddle-blade prop?> P-51B/C maybe D (+21 lbs/72") OR P-47D Razorback needle prop(to left?)?> Me-109G-6 (1.42 ata)> P-51D (+18lbs/67")> P-47D Bubbletop.

   The Hellcat and Corsair are somewhere near the FW-190A-8 wood prop, which is to say they can gain on the P-51D 30-40% on every 360° turn, and so can reverse a tailing P-51D (at 67" at least) in less than or near to 3X 360°... This MATCHES actual tests, anecdotes (up to a Honduran Soccer War account, of all things!), and the only thing in my above list that doesn't match a real test is...: The US Navy's test of the FW-190A-5 that is pegged as EQUAL to a P-51D at 1100° vs an A6M5's 2000° , CONTRARY to conventional wisdom... And STILL not good enough for me (I would expect 1300° at least if the A-8 is 1500-1600°, or if the FW-190A-4 can match turns with the P-38G, which British tests confirm it did)...

   So not specifying variant, power settings or propeller type just doesn't cut it.

   Except for one Luftwaffe La-5 evaluation, where a MW-50 Me-109 is said to out-turn an unknown FW-190A at an unknown speed (above 250 MPH I would guess), and another late-war test at 27 000 ft.+, where the Me-109G-14AS's superiority over the FW-190A-9 is very predictable, you will not find a single wartime statement where the Me-109G is accepted as turning better than the FW-190A...

   At the FW-190A's introduction, Gunther Rall came closest to saying the opposite vs his Me-109F, but his statement merely confirms that the FW-190A's turning superiority WAS A WIDELY ACCEPTED FACT: "They told us the FW-190A could out-turn our Me-109Fs... I, however(wry smile) could out-turn it..."

   Oh, and US 8th Air Force pilots also widely accepted that the FW-190A turned better than the Me-109, versus the ubiquitous 109G model at the very least, and there are numerous statements to that effect, and NONE that I know of to the contrary from British or US tests or pilots... As for the massive Russian combat evaluation I mention in this thread, I really wonder what room for interpretation it leaves:

   http://www.ww2f.com/russia-war/21828-russian-combat-experiences-fw-190-a.html


   Basically to ignore this you have to say: They don't really know what they are saying (like Johnny Johnson for instance), or... words don't actually mean what they mean... Or... Reality isn't really real...

   It's quite a gymnastic, and I am intimately familiar with it: I did the same for decades on end...

   Hopefully, one day the general consensus will try to go beyond deceptive appearances...

   Until then, if you want an accurate game comparison for some of these aircrafts, all I can do is offer you, for free, my recently updated, in full color, variant of Avalon Hill's "Air Force", a really intricate... Boardgame... E-mail me at : gaston1_01@hotmail.com

  Gaston

 

   

   

   

 

   

Offline Widewing

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #17 on: October 14, 2009, 06:12:14 PM »

   Spitfire Mk VIII/IX(+25 lbs)> FW-190A-8 wood prop> Me-109G-14 with MW-50> FW-190A-5> Spitfire Mk V OR P-47D Razorback paddle-blade prop?> P-51B/C maybe D (+21 lbs/72") OR P-47D Razorback needle prop(to left?)?> Me-109G-6 (1.42 ata)> P-51D (+18lbs/67")> P-47D Bubbletop.

   The Hellcat and Corsair are somewhere near the FW-190A-8 wood prop,

Geez Gaston, I'm glad you are staying away from armored vehicles, lest we see Sgt Rock being quoted as a source....

Can you explain how the heavier 190A-8 turns with an F6F, when an 190A-5/U4 was badly outclassed by the F6F and F4U in this test? http://www.wwiiaircraftperformance.org/fw190/ptr-1107.pdf


My regards,

Widewing

My regards,

Widewing

YGBSM. Retired Member of Aces High Trainer Corps, Past President of the DFC, retired from flying as Tredlite.

Offline Gaston

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #18 on: October 15, 2009, 01:54:37 AM »
  Well, first of all, the place I put the F6F/F4U in the list above DOES make them out-turn the FW-190A-5 significantly, just NOT by so large an amount as in the test you linked: I think an F6F 360° gain in 5-6 turns instead of 3 is more reasonable... The better-turning FW-190A-8, with wood prop, may in fact be equal to the F6F/F4U, if its low-speed performance against the P-51D is any guide (a 360° gain in 2-3 turns in some low-speed combat accounts, broad wood prop specified)...

  In the test you linked, the maneuverability results for the FW-190A-4 are mostly identical to the FW-190A-5 in the other, later A-5 test I used for reference:

  They AGAIN state that the F4U's roll rate is similar to the FW-190A-4! See what happened to the A-5 test below on this issue:

  In the particular FW-190A-5 I used to correlate the turn rates, this FW-190A-5 was fully dismantled and reassembled by the Allies, which was recognized as a bad mistake at the time, and this resulted in underperforming ailerons that the RAE contested with an official document during wartime, aimed at THAT particular test result, saying in effect the FW-190's roll rate was so superior it should NEVER be considered as equal to an F4U's roll rate, and that the US test was thus invalid in its conclusions... Imagine that: A roll rate argument... In wartime!

  Any Wartime FW-190A pilot will tell you the adjustement and choice of the FW-190A's ailerons were absolutely critical to its low-speed turn performance, allowing the aircraft to ride the stall better, with less "snapping" wing drop and thus less drag...

  Therefore these contested aileron results, by an actual Wartime document from the official test facility in the UK, also extend to the sustained low-speed turn performance of the aircraft in question...

  The fact that BOTH tests make the SAME mistake about the aileron performance show they are both invalid in the same way... There must have been something wrong with the way the Americans adjusted the ailerons. It's not me saying it: It's the British, during wartime!

  Note that DESPITE this handicap, the correlation of the F6F losing 360° from the A6M5 Zero in 3.5 X 360°, While the same A6M5, with the same pilot, gains on the P-51D 360° in about 1.8 X 360°, means that, since the FW-190A-5 loses 360° in 3 X 360° vs the F6F, the FW-190A-5 and the P-51D BOTH lose at the SAME rate versus the F6F or the A6M5...

  The F6F will gain 360° on the P-51D in 3X 360°, just like it did against the poorly reassembled FW-190A-5!

  If the A6M5 Zero turns 2000°; the F6F will do 1550°, the P-51D does about 1100-1190°, the "handicapped" FW-190A-5 will do 1180° or thereabout if the Navy test is to be believed (I don't, and I am sure it does at least 10-16% better)...

  So the FW-190A-5 (and A-4?) is EQUAL to the P-51D in low-speed turns FROM ACTUAL flight tests... Correlate the math: you will see it is correct, but take into account that the Army Zero tests required the A6M5 to gain only 180° to get on the tail of an Army fighter, while the Navy A6M5 Zero tests required the full 360°. (500 ft. Offset facing turn start for the US Army fighters, vs line astern for the US Navy fighters)

  So vs the Zero the P-51D lost-out in "less than a 360° turn", while the F6F lost out in "three and half 360° turns".

  I say the FW-190A-5 at low speeds should do about 14-20% better, gaining 360° on the P-51D in about five to seven 360° turns, while the FW-190A-8 should be 40% better, gaining 360° on the P-51D in about 2.5 360° turns (some actual combat accounts have it as low as two 360° turns with the broad wood prop, but I doubt these are correct or representative)...

  In any case, nobody accepts ANY FW-190As as equal-turning at low speeds to a P-51D, and yet the "handicapped" reassembled Navy test FW-190A-5, AND the A-4 test you linked, clearly shows them as equal to a P-51D in prolonged sustained turns, NOT high speed turns (where the P-51D's superiority is crushing).

  They are both gained on 360° by the F6F in the same number of 360° turns: 3.

  It's all there if you do the math...

  Gaston

  
« Last Edit: October 15, 2009, 02:13:15 AM by Gaston »

Offline Krusty

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #19 on: October 15, 2009, 02:04:38 AM »
The US test had badly aligned/adjusted trim tabs, and among other things this would ruin sustained turning (and probably explains noticable vibrations at a "mere" 350 knots). The British promptly took posession of the plane, readjusted it properly, and proved that the 190 performed better than they thought.

That aside, I don't see how a Spit8/9 is going to so significantly out-turn the Spit5 that it's got the 190s, the 109s, and the p47 between them in the rankings....

But.. er... not the 109G6??

 :headscratch:

That's just whack.

Offline Gaston

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #20 on: October 15, 2009, 02:42:00 AM »

  Quote, Krusty: "That aside, I don't see how a Spit8/9 is going to so significantly out-turn the Spit5 that it's got the 190s, the 109s, and the p47 between them in the rankings...."

   Well the Spifire Mk IX at +25lbs has such climb acceleration that it outclimbs everything else in WWII: How many people realize that? 4.2 minutes to 20 000 ft.! It even outclimbs the MK XIV at +18 lbs! The Me-109K does at best 4.8 minutes, or 4.5 with the contested 1.98 ata...

   To give you an idea, even the early Spitfire Mk IXs, when experimentally fitted as FLOATPLANES, had identical performance as their contemporary Mk Vs!!! THAT's how much extra power the Mk IX had....

  That kind of acceleration is paying dividents in the turn rate, just like it does for the Me-109G-14 with MW-50... Hartmann said the Me-109G could not compete on the Western Front without MW-50, and he was shot down the very first flight he flew after they took it out of his aircraft...

  The Me-109G-6 was about equal in turn rate to a P-51D, but slower on a smaller radius; this is actually not very good performance at all, but it DID match or beat the P-51D with the help of a downward spiral, especially if the P-51D didn't have the 72" boost from 150 Octane fuel...

  The Spit V varied greatly in available power. This may not apply to all: My ranking is based on this Johnny Johnson account:


   
    http://img30.imageshack.us/img30/4716/jjohnsononfw190.jpg


  Back on the 109 issue, the Hartmann comment does show you how laughable is ANY notion that the G-14 turns LESS well than a G-6....

  We do agree fully on these American FW-190A4/5 tests: Something just doesn't add up...

   Gaston
 

Offline Krusty

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #21 on: October 15, 2009, 03:09:14 AM »
Horsepower alone won't make a plane turn. Usually the higher powered planes are much heavier, and fight a lot more torque, and the lighter (slower) planes turn much better. Seems to be the case in almost every WW2 plane that gained power in later versions during the war,

Offline Angus

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #22 on: October 15, 2009, 03:26:55 AM »
I do have an account of a P51 ending in a sustained stall turn at tree-top level. With one notch of flap, the 51 out turned the 190. The 190 pilot took the clever way out, zoomed to a standstill and bailed.
Same allied pilot did however get into trouble with a 190. This was earlier, hence a lighter 190, and at the 190's optimum altitude. Spit pilot got away with a flick, where the 190 decided to leave.
Altitude is a key thing there, since the 190A series are optimized for low-medium.
BTW, Rall didn't fancy the 190 so much, untill the arrival of the Dora. But again, his playground was very high altitude in the west, and often top cover in the east.
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 Gaston

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #23 on: October 15, 2009, 04:18:34 PM »

  Quote: Angus: "I do have an account of a P51 ending in a sustained stall turn at tree-top level. With one notch of flap, the 51 out turned the 190. The 190 pilot took the clever way out, zoomed to a standstill and bailed."


    Yes, and I do know of another similar account, where the FW-190A's wingtip caught the three tops after being matched or slowly gained on by a Merlin P-51 in at least four consecutive on-the-deck 360° turns... Though in that account the speed might not have been sustained even with the 4 full 360° turns, as the speed at the moment it caught the threes was so high that the FW-190A STILL bounced on the ground and cartwheeled several times over a long distance, DESPITE the 4 consecutive 360° turns...

   Something to keep in mind is that usually all these three-top fights with escort fighters FOLLOW a continuous dive from 25 000 ft., so the speed at the start of turning could be extremely high, and still be well above 250 MPH after as many as four full 360° turns.

   You have to keep in mind the IMMEDIATE, and large, deterioration of the FW-190A's turn rate above 250 MPH, a speed still well below the maximum sustained turn rate ability of many other fighters. Above 400 MPH however, the disparity narrows down a little between most fighters, except apparently, in the 190A's case, to the right... (Also the FW-190A's disparity in high dive speed pull-outs is even larger still...)

   Another factor to consider is pilot experience, where in the case of one Merlin P-51 account, the FW-190A followed him around in a low speed turn, matching his turn rate, but according to the US pilot: "Snapping his wings all the way aroung the turn as he tried to follow"... The P-51 ended up the victor with flaps-down and the prop set on coarse pitch at very low speeds...

   This could be due to a lack of "patience" in fighter pilot's lingo: Trying to gain too much too quickly, and as a result constantly "catching" the FW-190A's violent wing drop all the time, and thus creating drag. This could easily happen due to overeagerness or a lack of pilot experience: Other aircrafts, such as the Spitfire, "rumbled" instead of snapping one wing violently down, and this may have been more "newbie"-friendly for getting maximum turn performance at low speeds.

   The final point that may cloud the issue is the FW-190A variant involved: The A-8 was THE major advance over all previous models, in both turn rate, initial level speed zoom and acceleration, yet that aircraft could often be a heavily armoured bomber-destroyer version. Even the use of four 20 mm cannons could make a big difference. The fact that Luftwaffe pilots cared about the FW-190A's low-speed handling is reflected by the VERY common removal of the outer 20 mm guns... Another major issue is the use of the broad-blade wood prop, which was a bit limited in availability even late in the war... So compare a four-20 mm guns FW-190A-6 at 1.42 ata with a narrow metal prop, or a two-20 mm gun FW-190A-8 at 1.58 ata with a broad wood prop, and it is a significant difference from some early 1944 accounts compared to some late 1944 ones...

   With the broad wood prop, this specialized low-speed turn fighter had little to fear apparently: "I feared no other aircraft in my FW-190A-8" said a FW-190A Western ace, an "ace" in P-51 kills, that would always, in his accounts, downthrottle below 250 MPH, and pop the flaps, to prepare AHEAD of a low-altitude fight with P-51s... The counter to "hit and run" tactics in this case would have been to force a series of head-to-heads, which usually favoured the FW-190A... "The FW-190A eagerly makes frontal attacks" as the Russian combat evaluation observed...

   As you can see in the ranking I made earlier in the thread, there is, from what I saw in 600 combat reports, little difference between a P-47D Razorback with paddle-blade prop and, say, a narrow-blade FW-190A-5. The Merlin P-51 should be MUCH worse than either with the flaps up, but as you will find in many accounts, it could become almost equal to earlier narrow-blade FW-190As, and even GAIN on Me-109Gs, by dropping the flaps and setting the prop pitch to coarse below 200 MPH. Here the Merlin's extra power at these low speeds allow it to maintain a stable speed even with the drag of the flaps that should be the downside of using flaps: Losing more speed than you gain in radius.

   This coarse-prop-pitch/flaps-down below 200 MPH is a very common, and successful, Merlin P-51 tactic at VERY low speeds (the flaps alone also help at high speeds), but in the words of one RAF Polish pilot, "It made the stall even more dangerous". I still don't think the Merlin P-51 could compete at all at low speeds with an optimized FW-190A-8 with wood prop, and even earlier FW-190As would give it trouble, especially with only two-20 mm guns and an experienced pilot...

   
   Quote Krusty; "Horsepower alone won't make a plane turn. Usually the higher powered planes are much heavier, and fight a lot more torque, and the lighter (slower) planes turn much better. Seems to be the case in almost every WW2 plane that gained power in later versions during the war."


   -It's not a simple cut-and-dried matter, but where turn RATE is concerned, more power WILL get you more turn rate, while lighter, lesser power planes will have a tighter RADIUS. Note that despite a generally crummy turn RADIUS, the Merlin P-51 often defeated the smaller turn radius of the Me-109G-6 with a better speed retention during a horizontal turn (a slight downward spiral helped the 109G-6 compete), resulting in faster turn RATE. But sitting on the "outside" of the 109's turn, P-51 pilots often describe having great difficulty "concluding" without stalling or "swinging" the nose inside their turn. (One P-51D pilot tells of almost stalling seven times on the deck, in a continuous turn, each time at the moment of firing, before finally hitting his late-war, probably MW-50-equipped, 109G target)

   The use of flaps is not such a great bonus, because what you get in radius you lose in turn rate...

   Turn rate is generally more tactically important than turn radius, which is why the notion of the MW-50 equipped Me-109G-14 being WORSE turning than the Me-109G-6 is so absurd...

   Gaston

   

 
   

   

   


Offline hitech

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #24 on: October 17, 2009, 09:11:53 AM »
Gaston: Wrote

Quote
by dropping the flaps and setting the prop pitch to coarse below 200 MPH.

This has to be one of the most backward statements I have heard.
Gaston: Do you understand how a constant speed props work? You statement is saying less HP is better when flying less than 200 MPH.

HiTech

Offline Widewing

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #25 on: October 17, 2009, 10:26:08 AM »
Gaston: Wrote

This has to be one of the most backward statements I have heard.
Gaston: Do you understand how a constant speed props work? You statement is saying less HP is better when flying less than 200 MPH.

HiTech

I was thinking the same thing; why would a pilot pull back the prop in combat??? The reality was that the throttle and prop went up and stayed up.

There were so many errors in Gaston's last post that I have no desire to spend an hour trying to correct them....


My regards,

Widewing
« Last Edit: October 17, 2009, 10:29:40 AM by Widewing »
My regards,

Widewing

YGBSM. Retired Member of Aces High Trainer Corps, Past President of the DFC, retired from flying as Tredlite.

Offline Gaston

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #26 on: October 18, 2009, 03:25:33 AM »

   If you say I am making errors without saying what they are, you're not giving me a chance to respond...

   Probably a lot of the disagreements have to do with the FW-190A supposedly not being an exclusive-horizontal-low-speed-turn-specialist, which is simulation-based nonsense that has nothing to do with what almost everybody in WWII ever said about them...

   As for the Merlin P-51 very low-speed down-throttling, with flaps down, and increased prop pitch settings (I said "coarser": sorry about that, but I think some of the pilots wrote the very same thing in their reports!), this is a very common tactic for the Merlin P-51s...

   Here is an example among many, a very interesting combat:

     http://www.spitfireperformance.com/mustang/combat-reports/339-hanseman-24may44.jpg

   
   Note he DID lower his throttle prior to out-turning the tailing Me-109G, and was being out-turned by it while the throttle was set higher...

   Gaston

Offline Angus

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #27 on: October 18, 2009, 03:40:11 AM »
More thrust at the same weight will give you a better sustained turn rate. How's that  :angel:
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 Gaston

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #28 on: October 18, 2009, 01:07:52 PM »

   Quote: "More thrust at the same weight will give you a better sustained turn rate. How's that"

   
     -Yes it does make more sense that way, but maybe the peculiarities of the Merlin P-51 airframe with flaps down require the lowering of the throttle. One of the stated advantages of the FW-190A's "brainbox" throttle is that it allowed downthrottling prior to the turn and then throttling up during the turn.

      In the Merlin Mustang's case, it does appear very clearly in the above combat that the lower airspeed increased the turn rate, probably at or below 200 MPH given the number of consecutive turns on the deck (while being gained on!),  and especially decreased the turn radius, to a far higher performance than higher speeds would have allowed.

     Yet at the same time, this 1990 test by several seasoned test pilots revealed a peak turn rate "very close" to the maximum level speed, which I read as above 300 MPH, maybe even as high as 350 MPH. I believe both are correct... Depending on flap position the turn behaviour of the Merlin P-51 is not really a linear rise followed by a linear drop...

     http://bbs.hitechcreations.com/smf/index.php/topic,261798.0.html

    As another example of Merlin P-51 peculiarities, the P-51 clearly accelerates or sustains speed better in level turns than earlier '44 Me-109Gs (not so much the late '44 one in the combat linked above!), yet cannot match their climb rates...

   In any case, it is obvious the lowering of throttle, and prop pitch change with popped flaps, during low speed turns, was a VERY common tactic on the Merlin P-51, and was widely known among US WWII pilots...

   Gaston

     

Offline Bronk

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Re: Turn rate hierarchy correlation from actual flight tests
« Reply #29 on: October 18, 2009, 01:33:58 PM »
So far I've got gaston throwing up a wall of text and hoping for something to stick.


.... Or have I not got the gist of it?
See Rule #4