Elevator control power is given by _____
(a) \(\frac{dCm}{d\delta e}\)
(b) Zero lift drag
(c) T = CD0 + K*CL
(d) DCL/ɑ
I had been asked this question at a job interview.
My query is from Longitudinal Static Stability and Control-2 topic in section Stability, Control, and Handling Qualities of Aircraft Design