Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics V-Symmetrically Tapered Wing with Circular Fuselage Having Horizontal and Vertical Tail. (Advance Restricted Report 3F23 June 1943)


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    Title :

    Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V-symmetrically tapered wing with circular fuselage having horizontal and vertical tail


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1943


    Size :

    15 pages


    Remarks:

    13 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :