Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Assessment of Modified 𝛾-Model for Hypersonic Boundary Layer Transition Prediction Considering Leading Edge Bluntness


    Contributors:

    Conference:

    AIAA International Space Planes and Hypersonic Systems and Technologies Conference ; 25. ; 2023 ; Bangalore



    Publication date :

    2023


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Bluntness-Dependent Hypersonic Boundary-Layer Modes’ Excitation

    Thele, Max / Selcan, Claudio / Sander, Tobias et al. | AIAA | 2022



    Effect of Slight Leading Edge Bluntness on Flat Plate Heat Transfer and Boundary Layer Transition at Hypersonic Mach Numbers

    Hozumi, K. / Nagai, S. / Fujii, K. et al. | British Library Conference Proceedings | 1994