By combining theory of linearized characteristics with hypersonic small disturbance approximation, explicit expressions are derived for shock shape, flow field, surface pressure distribution, and aerodynamic forces for delta wing and half-cone combination traveling at hypersonic speeds and small incidence; theory is applied to configuration for which surface pressure measurements are available; theoretical and experimental pressure distributions agree quite closely on body surface; but in wing-body junction and on wing, theory predicts pressures that are too low.


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    Titel :

    Theoretical study of inviscid hypersonic flow about conical flat-top wing-body combination


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Mandl, P. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 11


    Erscheinungsdatum :

    1964


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :