Flight-determined stability & control derivatives of supersonic aircraft with low aspect ratio unswept wing & t-tail


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    Title :

    FLIGHT-DETERMINED STABILITY AND CONTROL DERIVATIVES OF A SUPERSONIC AIRPLANE WITH A LOW-ASPECT-RATIO UNSWEPT WING AND A TEE-TAIL


    Contributors:

    Publication date :

    1959-04-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English