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 J Aeronautical Sciences v 17 n 9 Sept 1950 p 540-50, 594)


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    Title :

    Recurrence matrix solution for dynamic response of aircraft in gusts


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    90 pages


    Remarks:

    Diagrs, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English