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Applications of dynamic stability parameters to problems in aircraft dynamics

J. R. Chambers, D. J. Dicarlo, John L. Johnson

Abstract

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.

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Available abstract

Key concepts: Airplane, Aerodynamics, Stability (learning theory), Stability derivatives, Flight dynamics, Aviation, Spinning, Wind tunnel