problem 1:

Illustrate out the wing and aft tail contribution to the stick fixed static stability.

problem 2:

Discuss the phenomenon of the aileron reversal, adverse yaw, and steps to control adverse yaw and coupling between the rolling and yawing moments.

problem 3:

Quantitavely illustrate contribution of dissimilar components of aircraft towards directional stability and describe directional control.

problem 4:

Illustrate the rigid body equations of the motions of an airplane.

problem 5:

Illustrate out the term stability derivatives. Derive them.