Review of current structural design criteria, analysis methods, and data handling techniques is presented, summarizing practices that result in large discrepancies between design loadings and those that occur in flight; alternate criteria, methods, or research are suggested which eliminate these discrepancies; emphasis is on methods of providing structural integrity for flight in stall buffet regime, and rational method is derived for predicting empennage loads at stall; design loadings resulting from application of method are compared with loads measured during flight tests of large, swept-wing, high subsonic transport.


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    Title :

    Relationship between aircraft design and flight-measured loads


    Additional title:

    J Aircarft


    Contributors:
    Wittel, W.T. (author) / Disney, T.E. (author)

    Published in:

    Publication date :

    1967


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Relationship between Aircraft Design and Flight-Measured Loads

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