The application and analysis of dynamic stability parameters were examined. The effects of wing leading edge modifications on the stalling and spinning characteristics of a single engine general aviation research airplane are evaluated. It is illustrated how dynamic stability parameters measured in wind tunnel tests are used to predict the spin resistance of this class of aircraft, and that autorotation criteria are derived from the relationships which exist between static and dynamic aerodynamic characteristics.
Applications of dynamic stability parameters to problems in aircraft dynamics
1981-05-01
Conference paper
No indication
English
Experimental investigation on aircraft dynamic stability parameters
Tema Archive | 1993
|Dynamic Stability Characteristics of Aircraft and Dynamics of Pilot
Online Contents | 2004
|NTIS | 1981
NTIS | 1978