Free flight test of tailless missile configuration with 45-deg sweptback wing of aspect ratio 4 - stability at transonic speeds


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    Title :

    FREE-FLIGHT INVESTIGATION AT TRANSONIC SPEEDS OF THE STABILITY CHARACTERISTICS OF A TAILLESS MISSILE CONFIGURATION HAVING A 45 DEG SWEPTBACK WING OF ASPECT RATIO 4


    Contributors:

    Publication date :

    1956-08-28


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English