Influence of nonlinear effects on flight behavior of high-performance aircraft under control inputs is demonstrated with systematic calculations showing coupling effects with various symmetrical and unsymmetrical control inputs at different Mach numbers and altitudes; effects of changing aerodynamic derivatives, engine gyroscopic couple, and ratio of moments of inertia are demonstrated.


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    Title :

    Influence of deflection of control surfaces on free-flight behaviour of aeroplane


    Additional title:

    AGARD -- Report


    Contributors:
    Hafer, X. (author)

    Published in:

    Publication date :

    1961


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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