Prediction characteristics of separated turbulent boundary layers in compression corners used to determine aerodynamic heating distributions and dynamic loading of supersonic vehicles


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Length scale of separated turbulent boundary layers in compression corners.


    Contributors:

    Published in:

    Publication date :

    1966-08-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English