Adequacy of structure to withstand simultaneously loads and heating encountered in supersonic flight, examined by means of structural model; theory and attendant scaling laws for construction and testing of such aerodynamic heating models, having requisite similarity to any given aircraft flying any prescribed path, developed.


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    Titel :

    Theory of aircraft structural models subject to aerodynamic heating and external loads


    Weitere Titelangaben:

    NACA -- Tech Note


    Beteiligte:


    Erscheinungsdatum :

    1957


    Format / Umfang :

    48 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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