Schlieren photographs were used in an investigation to determine the effects of changing the aspect ratio from infinity to 2 on the air flow past a wing at high subsonic Mach numbers. The results indicated that the decreased effects of compressibility on drag coefficients for the finite wing are produced by a reduction in the compression shock and flow separation.


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    Titel :

    Effects of Aspect Ratio on Air Flow at High Subsonic Mach Numbers


    Beteiligte:
    W. F. Lindsey (Autor:in) / M. D. Humphreys (Autor:in)

    Erscheinungsdatum :

    1952


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch