Experiments conducted in supersonic wind tunnels during past 3 yr on missiles and projectiles show that pressure at base of bodies is essentially function of parameters that govern boundary layer; hence, base pressure is closely connected to surface friction and heat transfer phenomena; experimental results obtained in Naval Ordnance Laboratory supersonic tunnels at Mach 1.5-5.0 compared with theoretical results.


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    Titel :

    Interrelationship between boundary layer and base pressure


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Kurzweg, H.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1951


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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