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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    AIAA J


    Contributors:
    Mandl, P. (author)

    Published in:

    AIAA Journal ; 2 , n 11


    Publication date :

    1964


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :