Nah, if you’re not interested in the actual lift force because you’re just taking it for granted that the aircraft can generate the required lift coefficient and has sufficient thrust to overcome the resulting drag, there’s no need to worry about bank angle. You’re doing it right – what’s so wonky about 26deg/s in that scenario?

Yeah, sure. I assumed by the question he was looking at comparing corner speeds of different aircraft.

@ Inst [/QUOTE]This roughly indicates that if the F-22 is G-limited at 9G, it can perform 28 degree / sec turns at up to 650 km/h, or mach .56 at 15000 ft [/QUOTE]

It probably can but you need the E-M diagram to be sure of the aircraft envelope. BTW- you really don’t need to know the equations anymore, just go to one of the online pilot references that have turn rate calculators.