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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    Title :

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


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1957


    Size :

    48 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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