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This is what RAF BoB veteran, Spitfire ace & hugely experienced ( 550+ op sorties) combat fighter pilot
Bob Spurdle had to say about the P-40...
They had the flying characteristics of a brick."
Ol' Bob was a straight-shooting Kiwi, & used his P-40 well, to destroy a couple of Zeros over the Soloman Is,
"At over 20,000ft, a B-24, having dropped its bombs, could climb away from a Kittyhawk...
& this is exactly what happened."
I guess that after experiencing the climbing capabilty of a Spit IX, ol' Bob naturally found theYeah that is fine, but multiple other aces and hugely experienced, no-nonsense fighter pilots- Aussies Clive Caldwell (28 victories, 22 flying P-40s)...
The P-40 had an altitude ceiling of about ~16k' (Allison engined versions) or 20k' (Merlin engined versions) - it certainly performed poorly above that altitude.
I guess that after experiencing the climbing capabilty of a Spit IX, ol' Bob naturally found the
P-40 a tad pedestrian,
& he laughed at his fellow countrymen who enthused at what a 'hot-ship' it was, so I'm
guessing those other guys
hadn't..
Albeit, Bob commanded 80 Sqd RAF when they transitioned from Spits to Tempests,
& regarded the Spit IX as 'dainty', & 'feminine' - thereafter, what with the Tempest being much more - 'warlike' - n'all..
Here is my point, if the P40 burned off 150 gallons of fuel. It was 1000lbs lighter improving its nimbleness. This same thing played out for the next generation fighter the P51. Here no other aircraft caught up to the Mustangs muiltirole versatility and able to do them as well to far better than any other AC during WW2. That includes the new Jets. A mear 5 years later it would be a different story. Then again in Korea no other USAF plane was available for CAS.
Despite all the clamor the P47 would have done better. No...it was to way too heavy and slow on takeoff to be used on the short Japanese built airfields in South Korea. Plus would have taken twice the fuel load the Mustang would use for missions! It's large oil tank when hit would flame up like Corsairs. Especially the first year. But that is another story away from discussing the P40.
Another reason the P40 was useful because its flight mechanisms were well sorted out from its beginnings as a P36. The P38 was a nightmare in comparison. Taking 3 years to sort out the flight problems, bugs and nuances to make it a consistent effective fighting machine. Still after all the sorting the Mustang was still the dominant US fighter.
In the Pacific the Late model P40 had much better altitude performance against the Zero. Late model Zeros were heavier and less nimble though more capable with better guns and armor with a decent diving speed. Making them a fair match. Interesting watching YouTube where former Japanese aces described the Zero as an acrobatic plane and not a proper fighter. They very aware of its weaknesses and very brave pilots to fly those timber boxes. They further commented that the N1K2 as the first Japanese Navy to be on equal or better terms than the Americans.
Regarding the Zero...read Complete Book of WW2 Combat Aircraft - Military Press - Enzo Angelico and Paola Matricardi.
The late model P40 got the -81 to -117. The last 220 P40 built had a 1350 hp Allison.
One of the key attributes of a good fighter was Range and useful flight time! Here is where I think the Spitfire was over rated. Great performance but could not stay in the fight. That attribute was characteristic of every US plane other than the P39. All had decent to great range which made them successful because could fight in the enemy's neighborhood. All of the US planes were multifunctional as they were used as Recon, Fighter, bomber, fighter and liaison. Spitfire and Me109 carried limited fuel and ordinance to fight...
Hello a small note to Schweik's message, #609, already La-5FN was very capable plane, it had the same engine than La-7 but because the engine had better cooling in La-5FN, the engine in -5FN was clearly more reliable than in -7, even if it was somewhat draggier and so slower.
Actually all of the 1300 P-40K fighters some (I think ~200) of the later run P-40E had V-1710-73 rated officially at 1325 hp. The only real innovations on the V-1710-73 was automatic boost control and a stronger crankshaft which could handle the overboosting they were doing with the earlier models. 57" of boost became the standard WEP setting. From what I gather that could actually mean ~1500 hp at certain altitudes.
~ 300 of the P-40Ns (some of the early models as well as some of the later ones) had the 1350 or 1360 hp -1710-99 and -117
I think the -81 was a lower rated 1200 hp version used on the export / fighter-bomber variants of the P-40N and M
P-47's began replacing P-40's in the autumn of '43 in the MTO; by August '44, there was not a single P-40 with white stars in the theatre.
P-38's escorted 15th AAF bombers over Germany right up to the end of the war.
Generally true, but there were many different versions. Without touching the Spits with rear fuselage fuel tanks, Mk VIIs and VIIIs carried 121½ - 124 ImpGal fuel and had reasonable range but only the 140 high altitude Mk VIIs stayed in ETO, all Mk VIIIs were sent to MTO, CBI and Australia. And LR PR Spits could reach beyond Berlin from UK, even USAAF 8th AF used some PR Mk XIs. And Mk IX could carry 1000 lb of bombs as a FB, so they had some ordanance carrying capacity, even if not like e.g. Typhoon.
The -81 was outfitted 9.60:1 drive for supercharger. Result of that was improvement of altitude performance by some 10% above 14000 ft, the trade off being a loss of low-altitude performance by about same percentage. 1200 and 1325 HP power figures are for take off, that is a nice-to-have thing for a fighter, however the altitude power is more important, hence the engines similar to the -81 being better for the P-40s/39s/51s.
The real innovation for the -73 was strenghtening of some parts (crankshaft, or was it the crankcase?), allowing for greater boost and thus the power under 5000 ft (including take off power that was 1150 HP in previous types, like the -39). Both -39, -73 and similar engines were outfitted with 8.80:1 drive for supercharger.
at 3000rpm the supercharge impeller was spinning at 26,400rpm with 8.80 gears and with 9.60 gears you get 28,800.I never quite understood the 8:80:1 vs. 9.60:1 gearing issue. Can you elaborate on that a bit?
at 3000rpm the supercharge impeller was spinning at 26,400rpm with 8.80 gears and with 9.60 gears you get 28,800.
Power needed to drive the supercharger goes up with the square of the speed of the impeller which is where the early failure of the 9.60 gears comes from.
about a 17% increase in power needed.