Supersonic and hypersonic flow of inviscid ideal gas over conical delta wings using three dimensional method of characteristics


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    Title :

    A method for determining the complete flow field around conical wings at supersonic/ hypersonic speeds.


    Contributors:

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, FLUID AND PLASMA DYNAMICS CONFERENCE ; 1969 ; SAN FRANCISCO, CALIF.


    Publication date :

    1969-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :