Effect of Mach and Reynolds Numbers on Maximum Lift Coefficient Obtainable in Gradual and Abrupt Stalls of Pursuit Airplane Equipped with Low-Drag Wing. (Originally issued as Memorandum Report A5G06)


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    Title :

    Effect of Mach and Reynolds numbers on maximum lift coefficient obtainable in gradual and abrupt stalls of pursuit airplane equipped with low-drag wing


    Additional title:

    Advisory Committee Aeronautics -- Wartime Report


    Contributors:


    Publication date :

    1947


    Size :

    12 pages


    Remarks:

    Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :