An experimental investigation of the effects of Mach number and Reynolds number on the side forces induced on a slender body of revolution at high angles of attack was conducted. The tests were carried out in the Air Force Flight Dynamics Laboratory's Trisonic Gasdynamic Facility. (DePo)


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    Titel :

    An experimental investigation of steady asymmetric Vortex shedding from a slender body of revolution at high angles of attack


    Weitere Titelangaben:

    Experimentelle Untersuchung einer stationaeren asymmetrischen Wirbelabloesung bei schlanken Drehkoerpern und einem steilen Angriffswinkel


    Beteiligte:
    Turelli, R.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1977


    Format / Umfang :

    64 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch






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