It is shown that aerodynamic heating is reduced substantially by injecting small quantity of coolant into boundary layer; laminar boundary layer may be maintained at high supersonic speeds and high Reynolds numbers even with fluid injections.


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    Title :

    Analysis of supersonic aerodynamic heating with continuous fluid injection


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Klunker, E.B. (author) / Ivey, H.R. (author)


    Publication date :

    1949


    Size :

    31 pages


    Remarks:

    Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :