Niklas,
Actually it depends. I have that chart in the F4U-1 pilots manual. Notice the power varies with alt. and manifold pressure.
Notice when the F4U hits 60" of manifold pressure it is at 20,000ft. So that is also the alt where the modified F4U hit 65". But the changes in horsepower at that alt are much less because the lower air density reduces power output.
Take off 54" 2000HP Sea level
War emergency 57.5" 2250HP SL
" " 59.0" 2135HP 15,000FT
" " 59.5" 1975HP 20,000FT
These numbers are from the pilots manual. It is possible that the numbers are more conservative that was actual use of the A/C. But it still shows the higher the alt. the manifold pressure is checked the less effect it has on actual power output.
Also at the bottom of the page in which this data is printed, these numbers are not from flight test. The P-51B vrs F4U chart is from an actual flight test.
Later
F4UDOA