John Carrier wrote:
Generally, the sustained turn rate was around 14-15 degrees/second for
the F-4 hard-wing and about 12.5-13.5 for the F-105.
H'mm, those numbers seem kind of high for both, as far as sustained
capability
goes.
400 KTAS, turn rate in Deg./sec. (rounded off) = 19 (7g); 22 (8g).
500KTAS, turn rate in Deg./sec. (rounded off) = 15 (7g); 17 (8g); 20 (9g).
600KTAS, turn rate in Deg./sec. (rounded off) = 13(7g); 14 (8g); 16 (9g).
I'm missing something here. You say the numbers are high and then offer
higher numbers. Or are these just basic computations of turn rates w/o
regard to airframe factors?
snip
Yes. I wanted to show what the maximum turn rate was for the various KTAS/g
combinations; sustained would be less.
Guy
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