Question 1:
Illustrate out the wing and aft tail contribution to the stick fixed static stability.
Question 2:
Discuss the phenomenon of the aileron reversal, adverse yaw, and steps to control adverse yaw and coupling between the rolling and yawing moments.
Question 3:
Quantitavely illustrate contribution of dissimilar components of aircraft towards directional stability and explain directional control.
Question 4:
Illustrate the rigid body equations of the motions of an airplane.
Question 5:
Illustrate out the term stability derivatives. Derive them.