Investigation of distributions of pressure, recovery factor, and heat-transfer coefficient on 20° cones incorporating annular cavities was carried out in helium at free-stream Mach numbers of 11; effects of Reynolds number, cavity length-depth ratio, and reattachment region geometry were studied with emphasis on laminar, open cavity flow regime; results showed that pressure was virtually constant within cavity and downstream and very close to laminar attached-flow value.


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    Titel :

    Study of laminar hypersonic cavity flows


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Nicoll, K.M. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 9


    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





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