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    Title :

    Series solutions for shock tube laminar boundary layer and test time.


    Author / Creator :

    KING, W. S. /AEROSPACE CORP., LABS. DIV., EL SEGUNDO, CALIF./., MIRELS, H. /AEROSPACE CORP., LABS., DIV., AERODYNAMICS AND HEAT TRANSFER DEPT., EL SEGUNDO, CALIF./.


    Contributors:
    KING, W. S. (author)

    Published in:

    AIAA Journal ; 4 , 5 ; 782-789


    Publication date :

    1966




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English