Wind tunnel tests of static stability of model x-1e aircraft at mach 2 to 4


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    Title :

    WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01


    Contributors:

    Publication date :

    1959-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English