Determination of Stability and Control Characteristics of Straight-Wing, Tailless Fighter-Airplane Model in Langley Free-Flight Tunnel. (Advance Confidential Report L5K05)


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    Title :

    Determination of stability and control characteristics of straight-wing, tailless fighter-airplane model in Langley free-flight tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1946


    Size :

    16 pages


    Remarks:

    16 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :