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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Pressure response in supersonic wind-tunnel pressure instrumentation


    Additional title:

    J Applied Physics


    Contributors:

    Published in:

    Publication date :

    1953


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    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