Boundary layer transition for cooled 7.5 deg total angle cone at Mach 10


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental investigation of boundary-layer transition on a cooled 7.5 deg total-angle cone at Mach 10


    Contributors:

    Publication date :

    1967-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English