Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A Numerical Study of Nozzle Boundary Layer Thickness on Axisymmetric Supersonic Jet Screech Tones


    Contributors:
    Gao, Junhui (author) / Li, Xiaodong (author)

    Conference:

    12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference)



    Publication date :

    2006-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English






    Screech Tones of Supersonic Heated Free Jets

    Massey, K. C. / Ahuja, K. K. / Jones, R. R. et al. | British Library Conference Proceedings | 1994


    Effects of Jet Temperature and Nozzle-Lip Thickness on Screech Tones

    Hao Shen / Christopher K. W. Tam | AIAA | 2000


    Screech tones of supersonic heated free jets

    Massey, K. / Ahuja, K. / Jones, Jr., R. et al. | AIAA | 1994