NASA is embarked upon research and development tasks aimed at providing the general aviation industry with a reliable crashworthy airframe design technology. The goals of the NASA program are: reliable analytical techniques for predicting the nonlinear behavior of structures; significant design improvements of airframes; and simulated full-scale crash test data. The analytical tools will include both simplified procedures for estimating energy absorption characteristics and more complex computer programs for analysis of general airframe structures under crash loading conditions. The analytical techniques being developed both in-house and under contract are described, and a comparison of some analytical predictions with experimental results is shown.


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    Titel :

    Light aircraft crash safety program


    Beteiligte:
    Thomson, R. G. (Autor:in) / Hayduk, R. J. (Autor:in)

    Kongress:

    Business Aircraft Meeting ; 1974 ; Wichita, KS


    Erscheinungsdatum :

    1974-04-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Light Aircraft Crash Safety Program

    Thomson, R. G. / Hayduk, R. J. | SAE Technical Papers | 1974


    Crash safety in aircraft cabins

    Schuller, E / Sperber, M | AIAA | 1995


    Aircraft Crash Safety Research in Australia

    Sarrailhe, Stuart | SAE Technical Papers | 1983


    Crash safety tests of two transport aircraft

    Spicer, Jr., H.C. / Voyls, D.W. / Carroll, D.F. | Engineering Index Backfile | 1964


    Crash Safety Tests of Two Transport Aircraft

    Carroll, Donald F. / Voyls, Donald W. / Spicer, Herbert C. | SAE Technical Papers | 1964