Effects of Compressibility on Maximum Lift Characteristics and Spanwise Load Distribution on 12-FootSpan Fighter-Type Wing of NACA 230-Series Airfoil Sections. (Originally issued as Advance Confidential Report L5G10)


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    Title :

    Effects of compressibility on maximum lift characteristics and spanwise load distribution on 12-footspan fighter-type wing of NACA 230-series airfoil sections


    Additional title:

    Nat Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1945


    Size :

    13 pages


    Remarks:

    14 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :