Gents,
We have a flight model in the F4U-1C/D which is representative of the F4U-1A. Except up until now I never had the test data to prove it. Now thanks to Wells I have these documents and I can show our FM matches.
This data is a F4U-1A with water. It matches the current F4U-1D we have.
Here is the correct F4U-1D data
Notice
1. Initial climb is 3370FPM combat power and 2930FPM military power at 12,175LBS. Since climb and acceleration are tied together this mean a much better accelerating bird as well as a MUCH better climber.
2. Vmax at sea level in the clean condition is 366MPH and 417MPH at 20,000.
3. Notice how this data matches the Flight test against the P-51B, FW190A5, F6F-3/5 and A6M2/5 much better than the charts listed in AH.
4. Level stall at gross weight is 87.5mph.
The current AH FM stall is 100MPH.
It has been said be me and others that the prop change was largely responsible for the performance increase between the -1 and -1D.
This is apparently so as the -1 results use the blade design 6443 and the -1D uses 6501A-0.
5. Notice the design spec for the -1C is clearly a F4U-1D with a slightly heavier weight.
[This message has been edited by F4UDOA (edited 01-09-2001).]
[This message has been edited by F4UDOA (edited 01-09-2001).]