Wind tunnel tests of stability and control of variable sweep wing aircraft at Mach 1.97


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    Title :

    Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable-sweep Wings


    Contributors:

    Publication date :

    1960-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English