Boundary-layer transition on cooled 20° cone at mach numbers of 1.5 and 2.0.


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    Title :

    Boundary-layer transition on cooled 20° cone at mach numbers of 1.5 and 2.0


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    13 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :