Set of equations based on first mode of wing bending; representation of airplane is such that aerodynamic damping of vibratory motion of wing is separate from that of vertical motion of airplane as whole; easily evaluated solution of equations for unit jump forcing function is also presented which may be built up to determine response to any forcing function.


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    Title :

    Improved method for calculating dynamic response of flexible airplanes to gusts


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    13 pages


    Remarks:

    9 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English