Study of heat transfer measurements made in connection with studies on problem of calculating cooling requirements for supersonic aircraft.


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    Title :

    Comparison of theoretical and experimental heat transfer on cooled 20° cone with laminar boundary layer at mach number of 2.02


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Scherrer, R. (author) / Gowen, F.E. (author)


    Publication date :

    1950


    Size :

    18 pages


    Remarks:

    Diagrs, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :