CobberKane
Banned
- 706
- Apr 4, 2012
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I think the reason the P-47, as told by the pilots that flew it and against it in combat, talk about its incredible dive is energy. Though technically when tested by test pilots other planes could go faster, the Thunderbolt because of its own weight kept the energy from the dive and was able to convert it into climb. That and possibly because it had a better feel at those high speeds, giving the average pilot the confidence in his airplane. To a lesser extent, that may also explain the perception about the P-40 versus primarily the Japanese aircraft. It was much heavier and was able to retain its energy from the dive. Kind of like a heavier bullet retaining more energy down range than a lighter bullet.
Cobber - do you happen to have the RAE report that concluded that the Fw 190 and Bf 109 dove at a higher velocity than the P-47?
The myth that the P-47 wasn't a good climber was initially true when the narrow-chord props were used. Once they put on wide-chord props, the P-47 was still down a bit in low-altitude climb, but handily out-climbed many fighters at medium and especially high altitude. It was probably one of the best at 28,000 to 35,000 feet, right where many of them spent time on escort missions. Couple that with very good roll and you have a formidable escort aircraft.
The myth that the P-47 wasn't a good climber was initially true when the narrow-chord props were used. Once they put on wide-chord props, the P-47 was still down a bit in low-altitude climb, but handily out-climbed many fighters at medium and especially high altitude. It was probably one of the best at 28,000 to 35,000 feet, right where many of them spent time on escort missions. Couple that with very good roll and you have a formidable escort aircraft.
I think the highest figure the RAE ever got was mach .82 for a Spitfire, but the plane lost its prop and its wing were bent back in the process, though it still landed. I guess the effective critical dive speed probably would have been no more than the P 51.
Beginning in late 1943, high-speed diving trials were undertaken at Farnborough to investigate the handling characteristics of aircraft travelling at speeds near the sound barrier (i.e., the onset of compressibility effects). Because it had the highest limiting Mach number of any aircraft at that time, a Spitfire XI was chosen to take part in these trials. Due to the high altitudes necessary for these dives, a fully feathering Rotol propeller was fitted to prevent overspeeding. It was during these trials that EN409, flown by Squadron Leader J. R. Tobin, reached 606 mph (975 km/h, Mach 0.891) in a 45° dive. In April 1944, the same aircraft suffered engine failure in another dive while being flown by Squadron Leader Anthony F. Martindale, RAFVR, when the propeller and reduction gear broke off. Martindale successfully glided the Spitfire 20 mi (32 km) back to the airfield and landed safely. Martindale was awarded the Air Force Cross for his exploits.
A Spitfire was modified by the RAE for high speed testing of the stabilator (then known as the "flying tail") of the Miles M.52 supersonic research aircraft. RAE test pilot Eric Brown stated that he tested this successfully during October and November 1944, attaining Mach 0.86 in a dive