Discussion on experiment in which aerodynamic noise data at high Reynolds numbers obtained in supersonic speed range with aid of launch vehicle were telemetered from vehicle to ground recording station; results indicate shift in spectrum shape as function of Mach number, with higher frequencies corresponding to higher Mach numbers; it was also found that surface-pressure coefficients at supersonic Mach numbers do not vary markedly from those at subsonic Mach numbers for comparable flow conditions; study applicable to supersonic transport and launch vehicles.


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    Titel :

    Scout-vehicle aerodynamic-noise measurements


    Weitere Titelangaben:

    Sound


    Beteiligte:
    Hilton, D.A. (Autor:in)

    Erschienen in:

    Sound ; 2 , n 5 ; p 28-31


    Erscheinungsdatum :

    1963


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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