Analytic approximation is developed to determine temperature and thermal stress distribution; investigations show that results of existing thermal stress theories which neglect temperature gradient through skin thickness may exceed, in range of higher Biot numbers, true values by more than 30%; refined photothermoelastic experiments verify these results and add another significant conclusion, which is indicated.


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    Titel :

    Theoretical and experimental investigation of thermal stresses in hypersonic-aircraft wing structures


    Weitere Titelangaben:

    J Aerospace Sciences


    Beteiligte:
    Tramposch, H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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