OK sorry I'm on the rag, must be the turn rate BS on the general forum. Just be careful with blanket generalizations - P-38L engine is fairly insensitive to altitude while the P-51D power varies greatly.
Just did some tests, haven't even had time to analyze them:
15k feet altitude, WEP on, 100% internal fuel, max ammo.
Speeds in TRUE mph.
Speed (MPH TAS), P-38L time (SEC), P-51D time (SEC)
150,0,0
175,5,6
200,11,14
225,19,22
250,28,33
275,38,44
300,53,61
325,71,77
350,104,104
Same test, 20k feet.
200,0,0
225,8,9
250,18,19
275,29,30
300,43,46
325,60,62
350,87,88
I used TAS because as Pyro mentioned once, each plane has a different pitot tube calibration curve.
I just read the seconds of the stopwatch - not the tenths and hundredths, so error is +/- 0.5 second.
FYI 20k is the altitude where P-51D power begins it's second decline. If you get bored, Do 25k for me, should be a huge dropoff for the Mustang.
[This message has been edited by funked (edited 06-01-2000).]