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Anonymous
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DAVIDICUS said:RG_Lunatic:
Are you saying that the Spitfire XIV, Tempest, P-51B, and P-38 could exceed the P-47 in dive speed? I don't think so but at present can offer nothing more in support than what appears below.
The P-38 critical mach number was lower than that of the P-47, to it's max dive speed would be even lower.
It is important to understand that initial dive acceleration is a huge part of the "dive" performance. This is where the P-47 (and almost all US planes by virtue of their weight) excelled. At the start of the dive a P-47 could quickly pull thousands of feet away of a pursuer. After that, planes with higher critical mach figures would start to slowly catch up.
Also, critical mach figures usually indicate where the plane stops being responsive to controls, and often reflect wing and tail surface mach levels. At this point portions of the airflow over the plane such as the cowl and canopy might already be exceeding mach airflow, causing undesirable flying characteristics. The pursued plane would be less concerned with this than the pursuer, as he does not need to shoot.
Another important issue is terminal dive speed. Both the P-38 and the P-47 (and espeically the Me262) had serious terminal dive speed issues (where a dive could not be recovered and meant an inevitable crash), which were eventually "solved" through the use of dive recovery flaps. Dive recovery flaps had to be deployed at the beginning of a dive, once high speed was attained the hydrolics could not deploy them. These flaps had to reduce the critical mach figure for the planes and also acted as air brakes slowing dive acceleration.
Anyway, both the P-47 and the F4U were large planes with about the same relative power, so both would have had similar initial dive acceleration. The P-47N had a psuedo-laminar flow wing, so perhaps it's critical mach was equal to or higher than that of the F4U-4. Also, the F4U-4 had to be very careful above about 535 mph IAS or the fabric on the wings could be ripped off.
Attached is an interesting document concerning the behaivor of the Spitfire IX at high fractions of mach.
The 700 mph figure quoted is rubbish. Down low the air is just too thick for such speeds from a P-47 (and have the pilot survive), up high that exceeds mach 1. I suspect either the pilot was exagerating or the airspeed indicator was inaccurate at such high speeds (very likely). The maxium reading on the air speed indicator of the P-47 is 700 mph. Any dive steep enough to exceed much over 550 mph in a P-47 was probably terminal. A P-47 at 250 mph at 25,000 feet could not execute a normal power split-S without eating dirt!
=S=
Lunatic