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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    Title :

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


    Additional title:

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


    Contributors:

    Published in:

    Publication date :

    1977


    Size :

    64 Seiten


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English







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    Wu, G. / Beijing University of Aeronautics and Astronautics | British Library Conference Proceedings | 1994


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    MENDENHALL, M. / SPANGLER, S. / PERKINS, JR., S. | AIAA | 1979