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    Title :

    Comparison of the Minimum Drag of Two Versions of a Modified Delta-wing Fighter as Obtained from Flight Tests of Rocket-boosted Models and Equivalent Bodies Between Mach Numbers of 0.80 and 1.64


    Contributors:

    Publication date :

    1956-09-24


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English