A wind-tunnel investigation was conducted to determine the effect of wing planform on sonic boom at Mach numbers of 1.7, 2.0, and 2.7. The results of the investigation show that the wing leading-edge sweep is one of the primary planform variables affecting the overpressure characteristics.


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    Titel :

    Some Effects of Wing Planform on Sonic Boom


    Beteiligte:
    Hunton, L. W. (Autor:in) / Hicks, R. M. (Autor:in) / Mendoza, J. P. (Autor:in)

    Erscheinungsdatum :

    1973-01-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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