Wind tunnel tests on sonic boom with models of three wing-fuselage combinations


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    Title :

    A Wind-Tunnel Investigation at a Mach Number of 2.01 of the Sonic-Boom Characteristics of Three Wing-Body Combinations Differing in Wing Longitudinal Location


    Contributors:

    Publication date :

    1962-09-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English