Wind tunnel tests of delta wing space shuttle orbiter to obtain force and stability data at high angles of attack and blockage free conditions


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    Title :

    Space shuttle: Determination of static aerodynamic characteristics for the North American Rockwell delta wing orbiter at Mach numbers of 0.4 to 1.3


    Contributors:

    Publication date :

    1971-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :