SHOULD the P39 have been able to handle the Zero? Was it training or performance?

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What I get is that the tests were done (or at least written) about 2 months apart, in potentially different weather and with an engine that was going south compared to the first test, not to mention any other wear and tear on the aircraft.

While interesting any data has to be considered in that light.

I do like the note at the bottom where they say the XP-63A prototype showed a 110fpm difference in climb with and without pods and "Such a figure is close to the limites of climb determination accuracy".
 
If a Stuka initiates a turn too early, he gives the closing fighter a pretty easy (comparably speaking) deflection shot at fuel/pilot/engine. There was a reason that they converted to FW 190 as fast as they could.

I believe a fair number of the JU-87s were operating in a night attack role in the last few years of the war, JU-87Gs and a few others excepted which can skew the results as to losses. The FW 190s taking over the day attack role as you say.
 
Hi SR - good chart to discuss L/D and level flight characteristics.

Climbing (and turning) introduce Pressure Drag in a big way - mostly attributable to AOA caused Pressure Drag. In addition Cooling Drag escalated during climb and turn.

Total Drag = Parasite Drag (level flight components of Wing, fuselage, empennage, carb and Radiator ducts, gaps in control surfaces and sheet paneling, friction, exhaust stacks - stuff associated with basic airframe) + Delta Parasite Drag (more level flight components such as cannon/gun ports, radio mast, bomb racks, etc) + Vortex/Pressure Drag due to Angle of Attack = Total Drag (almost done).before Compressibility correction and addition of Induced Drag.

That said a full blown set of forces on the airframe have not yet been calculated. In late 1930s the concept of expressing practical climb, range and turn estimates required that many items be further categorized into attributes that contribute to Power Available and Power Required. This is where the esoteric calcs including equations for Ram Air, Prop design/configuration/efficiencies and Exhaust Thrust all contributed to Power Available as a function of altitude, velocity, throttle/manifold pressure, fuel type and fuel to air ratios.

.In WWII, at least for US airframe designers of piston engine fighters, the calculations for the Cooling drag of both cooling system and carb intake are derived into a delta Power Required.

For increments to Power Required, calcs for Cooling Drag factors for both high speed and low speed are derived from Wind Tunnel tests and also the increased drag due to the Prop Vortex (all fuselage, approx. 25-30% of wing) for the higher velocity than free stream and immersed in the vortex.

What emerges is the expression Thrust = Drag reorganized into Power Available and Power Required. In balance, there is equilibrium at top speed, top rate of climb, best turn rate, best cruise speed, etc. Otherwise, there is acceleration until equilibrium is once again attained
 
My date of 25 Dec 1943 was itself based on how long a new type aircraft which started to be produced in USA in Dec 1942 would actually be expected to be operational in UK. Shipping and training take much longer than you would think.
The first Thunderbolt combat mission is listed at 4/30/43 and was also the first 8thAF bomber mission with at least 100 planes.
 
Since most P-39s sent to Russia were the N and Q versions, is it possible these were quite well sorted as far as engine and CoG issues went while the earlier versions just shouldn't have been put into service?
Absolutely. After the P-400s were sent to Russia from the British, they began getting P-39Ns and Qs in ealy 1943. Almost all airplanes get better during production (initial bugs get sorted out etc) and the N was the ultimate version performance wise. The Q was just an N with gondola wing guns which hurt speed and climb. Since the Russians removed the wing guns on both they were basically the same plane.
 
The planes that the British got were not sorted then? especially in the area of tail shape/surface area and CoG

The planes delivered to England for test all had a modified non standard rudder.
Tested on the second British Airacobra (AH571) was a revised rudder of more angular shape and less area. Although the aircraft was delivered to England in this form, this rudder was not adopted as standard. A very small dorsal fin just ahead of the rudder became a standard feature of the RAF Airacobras and was also a distinguishing feature of the American P-39D and subsequent versions

CoG was adjusted again even on the P-39N
The 500 P-39Ns were followed by 900 P-39N-1s (Model 26C). These differed only in some minor internal changes which altered the location of the center of gravity.
 
Didn't VVS pre-war training feature a deficit of all kinds of practice, not just gunnery? Didn't the Japanese in Manchuria in 1938 point out some pilot proficiency deficits in the VVS?
Cheers,
Wes

I would say this was the case for most Allied pilots period. American, British, Australian, New Zealand, French, South African and Soviet. Gunnery training seemed to be rare, in fact it was very common for pilots right out of flight school to have barely enough training on their new (much higher performance) fighters to take off and land (and quite often, clearly not enough because there were a huge number of takeoff and landing accidents in the early years of the war especially in 1940-41)

S
 
 
I do get a little annoyed when you keep saying the British tried to get out of the contract. Have you got any evidence to support that, if so put it up or stop saying it.
Well, they DID get out of the contract with Bell and Lockheed. Whether it was Pearl Harbor causing a need for planes by the AAF or just refusal to accept, the British did not buy those planes. Lockheed just refitted the undelivered British order with turbos and handed propellers and they became P-38Fs.
 
Only one plane had the modified rudder etc. (SN AH-571) for the performance test.
 
Can you stop banging on about this, at the time the P39s were on the way to UK, the UK had loaded 40 Hurricane MkIIs and 550 mechanics/pilots to defend Murmansk. In total 3,000 Hurricanes and 1,400 Spitfires were sent. British and Canadian tanks shipped to Russia totalled over 5,000 and were first used in November 1941 on the Volga. The contract for 675 fighters is absolutely utterly insignificant in terms of cost. The significance really was they were available and crated up and of far more use to the USA and the Russians than they were to the British.
 
*SNIP*

Lockheed just refitted the undelivered British order with turbos and handed propellers and they became P-38Fs.
Or you know... they didn't and they actually were taken by the U.S.A.A.F. as the P-322-I and P322-II as advanced trainers ( 143 according to Wiki ). The rest of the French/RAF order were completed as P-38F's ( 420+/- ). Semantics perhaps but still...
 
I saw it (good post), now imagine you are the fresh faced bunch of pilots presented with your new steeds and one has a different tail to the others? Imagine you are the clients contract manager and you notice that this cut down version was the one tested?
 
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