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You can't trust these documents , it doesn't indicate who flew them or anything .I've read an article where a 2 RCAF pilots was showing evryone the capability of 109's and when one pilot flew against p38's he'd let them win because it was benificial when it came time to hit the bar/px . So some where out there is a document/report stating the the 109 was a dogAccording to the document the P-39 was a P-39C. If we trust wiki or joe baugher's site the P-39C had neither armor nor self-sealing fuel tanks and had two machineguns less than a P-39D. The weight advantage was ~400 pounds compared to P-39D.
There seem to be several transcription errors in this document, sometimes P-39 is written instead of P-38 or P-39D instead of P-39C and vice versa.
You can't trust these documents , it doesn't indicate who flew them or anything .I've read an article where a 2 RCAF pilots was showing evryone the capability of 109's and when one pilot flew against p38's he'd let them win because it was benificial when it came time to hit the bar/px . So some where out there is a document/report stating the the 109 was a dog
Was anybody else impressed or more appropriately, suprised, by the data in this particular test concerning the P39? The test states that the P39 is an even match for a Spitfire below 15,000 feet, not only out diving the Spitfire, but being faster, AND OUTCLIMBING THE SPITFIRE BELOW 15,000! I for one was flabbergasted when I read the test. Was anyone else?
http://www.wwiiaircraftperformance.org/P-40/PHQ-M-19-1307-A.pdf
Was anybody else impressed or more appropriately, suprised, by the data in this particular test concerning the P39? The test states that the P39 is an even match for a Spitfire below 15,000 feet, not only out diving the Spitfire, but being faster, AND OUTCLIMBING THE SPITFIRE BELOW 15,000! I for one was flabbergasted when I read the test. Was anyone else?
Why, if in this test the P39 is a match for the Spitfire below 15,000 feet, does nearly everone shake their head in disbelief at the Soviets stating that the P39 was a match for a 109 or 190 up to 20,000 feet after the wing guns and some of the armor have been removed?
The Air Fighting Development Unit received a British Airacobra I on July 30. They subjected it to tests and completed their report on September 22. They found the aircraft to be pleasant to fly and easy to takeoff and land. Controls were well balanced and although heavier than those of the Spitfire at normal speeds, did not increase appreciably in weight at high speeds as they did in the Spitfire.
It was difficult to hold the aircraft in a dive at high speeds unless the aircraft was trimmed nose-heavy. During a turn, the Airacobra would give ample warning of a high-speed stall by severe vibration of the whole airframe. Handling in formation and formation attacks was good, although deceleration was poor because of the plane's aerodynamic cleanliness. Take-offs and landings in close formation were not considered safe, since there was considerable difficulty in bringing the aircraft back to its original path after a swing.
The Airacobra I was powered by an Allison V-1710-E4 twelve-cylinder V in-line engine rated at 1150 hp for takeoff. Weights were 5462 pounds empty and 7845 pounds normal gross. Maximum speeds were 326 mph at 6000 feet, 343 mph at 10,000 feet, 355 mph at 13, 000 feet, 341 mph at 20,000 feet. Initial climb rate was 2040 feet per minute. With an internal fuel capacity of 100 Imp gal the Airacobra had an endurance of 1 hour 20 minutes at maximum continuous cruising speed at 6000 feet, 1 hour 5 minutes at 12,000 feet, and 1 hour 35 minutes at 20,000 feet. The true airspeeds at these altitudes were 287 mph, 327 mph, and 308 mph, respectively. Under most economical cruise conditions, the endurance increased to 3 hours 20 minutes, the relevant speeds being 183 mph at 6000 feet, 217 mph at 12,000 feet, and 215 mph at 20,000 feet. Under maximum continuous climb conditions, it took 15 minutes to reach 20,000 feet. The operational ceiling was considered to be about 24,000 feet, although there was a marked decrease in performance above 20,000 feet. At the Airacobra's rated altitude of 13,000 feet, it was 18 mph faster than the Spitfire VB. However, the speed fell off rapidly above that height, and the two planes were almost exactly matched at 15,000 feet. At 20,000 feet, the Spitfire VB was 35 mph faster and at 24,000 feet it was 55 mph faster. The ground run of the Airacobra during takeoff was 2250 feet, as compared with 1470 feet for the Hurricane II and 1590 feet for the Spitfire V.
The AFDU also did some comparative dog-fighting tests with the Airacobra against a Spitfire VB and a captured Messerschmitt BF 109E. The Airacobra and the Bf 109E carried out mock dog-fighting at 6000 feet and 15,000 feet. The Bf 109E had a height advantage of 1000 feet in each case. The Bf 109, using the normal German fighter tactics of diving and zooming, could usually only get in a fleeting shot. The Bf 109 could not compete with the Airacobra in a turn, and if the Bf 109 were behind the Airacobra at the start, the latter could usually shake him off and get in a burst before two complete turns were completed. If the Bf 109 were to dive on the Airacobra from above and continue the dive down to ground level after a short burst of fire, it was found that the Airacobra could follow and catch up to the Bf 109 after a dive of over 4000 feet. When fighting the Bf 109E below 20,000 feet, the Airacobra was superior on the same level and in a dive.
A similar trial was carried out against a Spitfire V. Although the Airacobra was faster than the Spitfire up to 15,000 feet, it was outclimbed and out-turned by the Spitfire. Unless it had a height advantage, the Airacobra could not compete with the Spitfire. If on the same level or below, at heights up to about 15,000 feet, the Airacobra would have to rely on its superior level and diving speeds and its ability to take negative "G" without the engine cutting out. Above 15,000 feet, the Airacobra lost its advantage in level speed.
The Airacobra was considered to be very suitable for low altitude operations because of the excellent view and controllability, and it was fully maneuverable at speeds above 160 mph.
Why the Soviets were not allowed to use the P-63 against Germany?
To me it would make sense that they would use the Canadian Built HurricaneI wonder what Spitfire and Hurricanes were tested? There is no indication to sub-types in the documentation.
AFAIK, the US had access to a Spitfire Mk I and two Spitfire Mk VA that they'd used for testing. The Mk Vs arrived in April 1941.
Anyone know what Hurricanes were flying in the US in 1941?
I imagine it would be because the Spitfire used for comparison used a single speed single stage Merlin with a higher rated altitude than the Allison in the P-39, giving better altitude performance at the expense of low altitude performance.
Thoughts?