Airplane aerodynamic moments, equilibrium, static stability, control characteristics in steady flight, and dynamic longitudinal and lateral stability are discussed. The aerodynamic center and moment about the aircraft of the wing with fuselage and nacelles; equilibrium in steady, symmetric straight flight; static longitudinal stability with stick free and fixed; longitudinal control in pull up maneuvers and steady turns; steady, asymmetric flight; and the equations of motion of an airplane are covered.
Lecture Notes on Airplane Stability and Control 1, Part 1
1983
268 pages
Report
No indication
English