Analytical evaluation of these forces and response of flexible airplane to continuous turbulence in supersonic flight by applying power-spectral-density (PSD) method; aerodynamics for supersonic flight is described in terms of lifting-surface theory represented by linear integral equation; development is carried out for airplane with coplanar wings of arbitrary plan-form subjected to random vertical turbulence description; by applying box technique, aerodynamic influence coefficients are obtained for combined elastic response and gust excitation velocity potential, which in turn determines, aerodynamic loads and generalized forces; statistical results and definition of parameters obtained by PSD method.


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    Title :

    Unsteady aerodynamics and dynamic response of flexible supersonic aircraft to continuous turbulence


    Additional title:

    J Aircraft


    Contributors:
    Ii, J.M. (author) / Sidwell, K.W. (author)

    Published in:

    Publication date :

    1968


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :