Investigation to determine performance of simple thin airfoils with aid of nonlinear transonic theory first developed by T.vonKARMAN; expressions for pressure coefficient across oblique shock and Prandtl-Meyer expansion are developed in terms of transonic similarity parameter; aerodynamic coefficients calculated in similarity form for flat plate and asymmetric wedge airfoils, and curves are plotted.


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    Titel :

    Airfoils in slightly supersonic flow


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Tsien, H.S. (Autor:in) / Baron, J.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1949


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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