Shock tube test time limitation due to premature arrival of contact surface is analytically investigated for wholly turbulent-wall boundary layers; results are compared with those for wholly laminar-wall boundary layers; results are presented in nondimensional form so as to be applicable for arbitrary initial pressures and tube diameters; criteria are established to define when turbulent-wall and when laminar-wall boundary-layer theory is applicable; present solution is intended for case where wall boundary layer introduces sizable reductions in test time.


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    Titel :

    Shock tube test time limitation due to turbulent-wall boundary layer


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Mirels, H. (Autor:in)

    Erschienen in:

    AIAA Journal ; 2 , n 1


    Erscheinungsdatum :

    1964


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :