Nozzle wall hypersonic boundary layers in helium tunnel, presenting skin friction measurements and heat transfer rates


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    Title :

    Nozzle wall boundary layers at Mach numbers 20 to 47


    Contributors:

    Conference:

    AEROSPACE SCIENCES MEETING ; 1971 ; NEW YORK, NY


    Publication date :

    1971-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Nozzle Wall Boundary Layers at Mach Numbers 20 to 47

    JOSEPH H. KEMP AND F.K. OWEN | AIAA | 1972


    Nozzle wall boundary layers at Mach numbers 20 to 47

    KEMP, JR., J. / OWEN, F. | AIAA | 1971



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