Problem relating to development of aircraft, rockets, etc; due to lack of knowledge as to parameters in design of pressure instrumentation, response time has been known to exceed running time in case of intermittent tunnel; analysis of systems connected in series.


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    Titel :

    Pressure response in supersonic wind-tunnel pressure instrumentation


    Weitere Titelangaben:

    J Applied Physics


    Beteiligte:
    Ducoffe, A.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1953


    Format / Umfang :

    12 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Instrumentation of the Ames Supersonic Free-flight Wind Tunnel

    Briggs, Robert O / Kerwin, William J / Schmidt, Stanley F | NTRS | 1952


    Instrumentation of the ames supersonic free-flight wind tunnel

    Briggs, Robert O. / Kerwin, William J. / Schmidt, Stanley F. | TIBKAT | 1952


    Pressure Fluctuation Measurements in the NAL 0.2-m Supersonic Wind Tunnel

    Sawada, H. / Kohno, T. / Kunimasu, T. et al. | British Library Conference Proceedings | 1998



    Pressure fluctuation measurements in the NAL 0.2-m supersonic wind tunnel

    Sawada, Hideo / Kohno, Takashi / Kunimasu, Tetsuya | AIAA | 1998