Procedure developed for calculation of structural response of airplane subject to dynamic loads; particular attention given to problem of determining stresses developed due to flight through gusts. (See also Nat Advisory Committee Aeronautics -- Tech Note n 2060 Mar 1950 90 p)


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    Title :

    Recurrence matrix solution for dynamic response of aircraft in gusts


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1950


    Remarks:

    Diagrs, tables


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English