Research program on low-speed aerodynamics as applied to STOL and VTOL aircraft conducted by Cornell Aeronautical Laboratory; paper presents experimental data on airfoil maximum lift in 2-dimensional shear stream and theoretical studies devoted to explaining these results; experimental data showing destalling phenomena are discussed, and results of theoretical studies presented to illustrate effects of shear on airfoil stall.


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    Titel :

    Influence of two-dimensional stream shear on airfoil maximum lift


    Weitere Titelangaben:

    J Aerospace Sciences


    Beteiligte:
    Vidal, R.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    16 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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