Hi Elvis,
>In post #73, Ju Ha wrote the following as part of that post...
>That works out to 25.7+ deg./sec.
>Why the differences in those figures compared to yours?
I guess that the higher figure is for a combat turn that sustains altitude, but not speed.
I calculate a sustained turn speed of about 240 km/h TAS, while 350 km/h IAS (calibrated, I assume) works out to 386 km/h TAS. At that speed, the F2A according to my calculations is capable of a 40 degrees per second turn, pulling 7.7 G and decelerating with 6.6 m/s^2. (The deceleration of course reduces G rate, turn rate and further deceleration, so I'd say like my calculations are in the same ballpart for a decelerating turn as those Juha quoted.)
In my opinion, the figure of 350 km/h is what we'd consider "corner speed" in modern technology - the speed at which the F2A can generate the highest instantaneous Gs that can be usefully employed to combat, limited by airframe strength or by the pilot's ability to resist G forces. That's probably the reason it's listed for 180 degrees of turn - if attacked by an enemy from astern, you could make such a turn from corner speed to spoil his attack, and after 180 degrees you'd probably be facing him head-on (depending on the timing of the turn, of course).
A sustained turn at 350 km/h IAS would be much tamer and have a much wider radius - I calculate 14.5 degrees per second compared to the 23.3 degrees per second at 240 km/h TAS for highest sustained turn rate.
Regards,
Henning (HoHun)
>In post #73, Ju Ha wrote the following as part of that post...
>That works out to 25.7+ deg./sec.
>Why the differences in those figures compared to yours?
I guess that the higher figure is for a combat turn that sustains altitude, but not speed.
I calculate a sustained turn speed of about 240 km/h TAS, while 350 km/h IAS (calibrated, I assume) works out to 386 km/h TAS. At that speed, the F2A according to my calculations is capable of a 40 degrees per second turn, pulling 7.7 G and decelerating with 6.6 m/s^2. (The deceleration of course reduces G rate, turn rate and further deceleration, so I'd say like my calculations are in the same ballpart for a decelerating turn as those Juha quoted.)
In my opinion, the figure of 350 km/h is what we'd consider "corner speed" in modern technology - the speed at which the F2A can generate the highest instantaneous Gs that can be usefully employed to combat, limited by airframe strength or by the pilot's ability to resist G forces. That's probably the reason it's listed for 180 degrees of turn - if attacked by an enemy from astern, you could make such a turn from corner speed to spoil his attack, and after 180 degrees you'd probably be facing him head-on (depending on the timing of the turn, of course).
A sustained turn at 350 km/h IAS would be much tamer and have a much wider radius - I calculate 14.5 degrees per second compared to the 23.3 degrees per second at 240 km/h TAS for highest sustained turn rate.
Regards,
Henning (HoHun)