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Old 15th Feb 2021, 07:40
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PEL
 
Join Date: Mar 2009
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Thrust Vectoring Effect on Rate of Turn
Hi everyone

I just got a question after reading my old POF book. the Eqaution for rate of turn: ROT = 1,091 x tangent of the bank angle / airspeed

How would that change when the airplane is equipped with Thrust Vectoring?? like the F22 og SU35???? Does anyone has an equation for that??
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