Wind-tunnel tests of rectangular Clark Y wing made with N A C A spinning balance; all six components of aerodynamic force and moment were measured throughout range of angles of attack and angles of sideslip, likely to be attained by spinning airplane; application of data from spinning balance to estimation of angle of sideslip necessary for spinning equilibrium at any angle of attack. (Price 10¢)


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    Title :

    Spinning characteristics of wings. I -- Rectangular Clark Y monoplane wing


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1935


    Size :

    20 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :