Swept wing fighter aircraft drag coefficient reduction by configuration redesign


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    Title :

    Minimum Drag of Four Versions of a Swept-wing Fighter Airplane Obtained from Flight Tests of Rocket-boosted Models at Mach Numbers from 0.81 to 1.71


    Contributors:

    Publication date :

    1956-09-07


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English