Transition characteristics were determined for smooth, blunt nosed cones varying from 27 to 60° in included angle; Mach number effects were small for small bluntnesses but increased for larger; strongest effect was in Mach number range 1.61 to 1.82; increase in nose bluntness caused decrease in transition distance and transition Reynolds number.


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    Titel :

    Effects of cone angle, Mach number, and nose blunting on transition at supersonic speeds


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Czarnecki, K.R. (Autor:in) / Jackson, M.W. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    31 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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