Structural Analysis of the flap, aileron, wing fan closure doors, wing trailing edge, and wing fittings for the U.S. Army XV-5A lift fan research aircraft are presented in this report. For each component, a summary type analysis is presented primarily with the intent of giving structural configuration, final critical loading, and assumptions made. Structural proof tests were conducted satisfactorily on the basic wing, the fan doors, fan fittings, flap and aileron. (Author)


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    Title :

    Structural Analysis of Wing Secondary Components


    Publication date :

    1963


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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