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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    Titel :

    Relationship between aircraft design and flight-measured loads


    Weitere Titelangaben:

    J Aircarft


    Beteiligte:
    Wittel, W.T. (Autor:in) / Disney, T.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Relationship between Aircraft Design and Flight-Measured Loads

    W. T. WlTTEL AND T. E. DlSNEY | AIAA | 1967



    Analysis of Measured In-Flight Tail Loads

    Van Gelder, P. A. | British Library Online Contents | 1996


    Analysis of Measured In-Flight Tail Loads

    Van Gelder, P. A. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1996


    Analysis of Measured In-Flight Tail Loads

    P. A. van Gelder | NTIS | 1996