Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Flight test base pressure results at hypersonic Mach numbers and highReynolds numbers in turbulent flow - Implications to ground test simulation requirements


    Contributors:

    Conference:

    9th Aerospace Sciences Meeting ; 1971 ; New York , NY , U.S.A.



    Publication date :

    1971-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





    Role of Turbulent Prandtl Numbers on Heat Flux at Hypersonic Mach Numbers

    Xudong Xiao / Jack Edwards / Hassan Hassan et al. | AIAA | 2007



    Documentation of crossflow transition in flight at hypersonic Mach numbers

    Bertelrud, Arild / Graves, Sharon / Young, Ronald et al. | AIAA | 1995


    Transition measurements at hypersonic Mach numbers.

    Henderson, A., Jr. / Maddalon, D. V. / Rogallo, R. S. | NTRS | 1967