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.


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    Title :

    Applications of dynamic stability parameters to problems in aircraft dynamics


    Contributors:


    Publication date :

    1981-05-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Applications of dynamic stability parameters to problems in aircraft dynamics

    Chambers, J. R. / Dicarlo, D. J. / Johnson, J. L., Jr. | NTRS | 1981


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    Fusco, F. / Guglieri, G. | Tema Archive | 1993