Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Effect of Mach number on boundary layer noise


    Contributors:

    Conference:

    20th AIAA/CEAS Aeroacoustics Conference



    Publication date :

    2014-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    A High Mach Number Turbulent Boundary-Layer Study

    E. Backx / B.E. Richards | AIAA | 1976




    Application of Boundary Layer Combustion in High-Mach-Number Scramjets

    Peng, Yuan / Xu, Jinglei / Chen, Kuangshi | AIAA | 2024


    Optical refraction from high Mach number turbulent boundary layer structures

    Erbland, P. / Etz, M. / Lempert, W. et al. | AIAA | 1998