davparlr
Senior Master Sergeant
Another factor to consider in any discussion of the relative merits of F4U4 and the P51 H is that the F4U4 had a service ceiling of 41400 ft so it was no slouch at getting up there and it's critical altitude was 26200 ft where it got it's 446 mph TAS. From a practical point of view I wonder how much acm with recip engines took place at altitudes above 30000 ft. Other factors to consider might be controllability and ammo load. I have read in a number of places that the Mustang could be a handful in certain flight regimes whereas the Corsair had the reputation of being a sweet handling plane in the air with excellent control force modulation throughout. The Corsair of course had an ammo load of 2350 rds of 50 cal. I wonder what the H carried. By the way, it is my understanding in a turning fight the Corsair was improved vastly by 10 or 15 degrees of flap. Corsair turning ability was impaired by the right wing spoiler which more or less cured the left wing drop. I read somewhere that Hub Zemke spent time in a LW POW camp because he lost a wing on his P51 in a thunderstorm. As you said for long range fighter escort the P51 was the obvious choice. For a carrier capable fighter the Corsair hands down. For all the other roles except possibly the interceptor job, seems to me the Corsair comes out on top.
The only maneuvering problem I have heard of for the P-51 was if the pilot failed to use his aft tank of gas first. This moved the cg aft and caused handling problems. Also, stall characteristics could be exciting. However, a Mustang pilot should always avoid low speed maneuvering since his advantage was always at high speed.
The '43 P-51B was at a disadvantage to the F4U-1 except above 25k. The '44 P-51B was significantly faster than the F4U-1 at all altitudes and is actually close to the F4U-4. The P-51D had airspeed advantage over the F4U-1 except between 15 and 20k. In maneuvering, the F4U-1 has wing loading and power loading advantage. The P-51H was faster at altitudes than the F4U-4, significantly faster below 15k (over 30 mph at SL and 40 mph at 5k). In addition, the P-51H has a power loading advantage. Wing loading is a slight advantage for the F4U-4.
So, nose to nose,
F4U-1 has advantage over '43 P-51B below 25k. Naval comparison test confirm this comparison. Test also revealed that the P-51 had a much superior dive speed than the F4U.
'44 P-51B has advantage over F4U-1 at all altitudes (due to much greater level speed and dive speed)
P-51D and F4U-1 pretty well even with speed advantage for P-51 over most of the envelop up to 25k, but better maneuvering for F4U-1. Above 25k, the P-51 would have the advantage. Again, P-51D would have superior dive speed.
P-51H has advantage over F4U-4 below 15k due to much higher level speed advantage. Above 15k they are pretty equal with the P-51H having an airspeed advantage and power loading advantage but the F4U-4 having better wing loading. Both planes climb superbly with the F4U-4 having a slight advantage. Again, P-51H would have superior dive speed. Also, two thousand pound weight advantage would certainly benefit the P-51H in sustained turns.
The Joint Fighter Conference perfered the P-51 to the F4U-1, although very close below 25k.
As to losing a wing in a thunderstorm, many an aircraft has come out of a thunderstorm in pieces. Thunderstorms are dangerous to all aircraft and have to be avoided. We lost a C-141 over England in one. The plane had lost its radar. Later analysis indicated that it got into vertical down draft of 6000 ft/min immediately followed by an updraft of 6000 ft/min. The engines pulled off the wings.