Nozzle boundary layer displacement thickness at Mach 30-70 in helium using Langley hotshot tunnel tests


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    Title :

    Nozzle boundary-layer displacement thickness at Mach numbers 30 to 70


    Contributors:

    Publication date :

    1969-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English