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Corsair wins.
I did a quick search and couldn't find an existing thread, so...
Which is the better aircraft? I will not be posting much data as I 1) am not that knowledgable technically, so this should be good and 2) I'm here to learn, and I don't have access to all the resources some of you guys have.
Personally, I'm partial to the F4U, but this thread is NOT here to choose favourites, but rather to determine which the better plane was and why. Have at 'er!
Drgondog,
What is 3-1-1 and 4-1-1?
Is it 3 kills, 1 damaged, 1 probable?
The airplane that is most ignored in these discussions is the P51B-15 with Malcom Hood and the 1650-7 engine on 44-1 fuel. Only the P-51H is superior Mustang variant.
My father got 3-1-1 in the air in his first two weeks in this bird, then converted to a P-51D and got 4-1-1 for the next 10 months. He always had a great affection for acceleration, climb and turn performance in that B-15 over all variants of the P-51D
But performance of the F4U-1 at alt was much better than the the contemporary Fw 190A, and some 109's. (and still compeditive with most contemporary 109's)
As it was the P-51B made a much better escort fighter -particularly fo the higher flying B-17's- but if there had been separate development of the F4U for the AAF, a higher altitude supercharger would likely have been used sooner if not a turbocharged variant.
Here's an interesting discussion on this we had going a while back: http://www.ww2aircraft.net/forum/aviation/battle-over-germany-january-1944-a-13336.html
I certainly agree with this. I selected this aircraft as the one I would most like to fly if I had to fly in WWII, on another thread. This aircraft, at fighter weight of 8500 lbs. could be quite competitive with even the latest German aircraft, besting the Fw-190D-9 at almost all altitudes in speed and probably equal in climb, if the D-9 would have to be lowered to some fighting weight to be competitive. The Bf-109K and the Ta-152H would have to be dealt with carefully as they had some performance edge, although not a lot up to 25k.
It is also interesting to note that if they had dropped the -9 engine in the B, or even D, performance would have been very near the P-51H, the B being closer since it is lighter than the H. I would think that change would have been no more complex than the other engine upgrades. They just didn't need to do it.
Dave - I agree the similarities that would have occurred between the B and the H after dropping the 1650-9. The D was still about 600 pounds heavier empty than the B and 500 heavier thn the H. The D would have of course climbed and accelerated better but I'm sure it would not have matched the 51B with the 1650-3 or -7.
actually the -9 was very similar to the -3 but beefed up to take the much higher boost so it weighed about 50 pounds more but externally, mount wise it was same.
As for comparing the P-51 to the F4U, they were designed for different missions. Neither aircraft could perform the other mission better. The F4U-1 would not have been able to provide the coverage necessary to protect the bombers in early to late '44. While their range was adequate, performance dropped off significantly above 25k, allowing the enemy to attack from above. The F4U-4 could perform at altitude but lacked internal fuel range and if they were added, the F4U-4 would still have missed the critical time for bomber escorting. While the P-51 could probably been upgraded to carrier quals, the added weight would have hindered performance even more at lower altitude, where it was not designed to play. In addition, the liquid cooled design would have made carrier maintenance more complex.