Analytical procedure used to modify design of high-pressure-ratio nozzles to reduce vibration during start-up and shutdown. Nozzles used in jet engines, laser nozzles and diffusers, wind tunnels, gas turbines and rocket engines.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Supersonic-Nozzle Shock-Wave Analysis


    Contributors:

    Published in:

    Publication date :

    1984-11-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Supersonic shock wave nozzle decompression device

    WANG YONGQING / PAN YING / CHEN ZHONGMING et al. | European Patent Office | 2024

    Free access

    Unsteady Pressure-Sensitive Paint Measurement for Oscillating Shock Wave in Supersonic Nozzle

    Nakakita, Kazuyuki / Osawa, Junichi / Hori, Nobuaki et al. | AIAA | 2008


    Unsteady Pressure-Sensitive Paint Measurement for Oscillating Shock Wave in Supersonic Nozzle

    Nakakita, K. / Osawa, J. / Hori, N. et al. | British Library Conference Proceedings | 2008


    Shock Motion and Flow Instabilities in Supersonic Nozzle Flow Separation

    Johnson, Andrew / Papamoschou, Dimitri | AIAA | 2008


    Shock wave noise of supersonic aircraft

    Ryhming, I.L. / Yoler, Y.A. / Aoki, Y. | Engineering Index Backfile | 1960