Experimental Determination of Yawing Moment Due to Yawing Contributed by Wing, Fuselage, and Vertical Tail of Midwing Airplane Model. (Advance Restricted Report 3F28 June 1943)


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    Title :

    Experimental determination of yawing moment due to yawing contributed by wing, fuselage, and vertical tail of midwing airplane model


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1943


    Size :

    12 pages


    Remarks:

    5 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :