The paper presents highlights of a recent study which illustrates the application and analysis of dynamic stability parameters. More specifically, the investigation consisted of an evaluation of the effects of wing leading-edge modifications on the stalling and spinning characteristics of a single-engine general aviation research airplane. The results of the investigation illustrate 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 can be derived from the relationships which exist between static and dynamic aerodynamic characteristics.
Applications of dynamic stability parameters to problems in aircraft dynamics
Lecture Series on Dynamic Stability Parameters ; 1981 ; Moffett Field, CA, US
1981-03-01
Conference paper
No indication
English
Experimental investigation on aircraft dynamic stability parameters
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