Report of Lewis Flight Propulsion Laboratory is useful in gas turbine system cooling.


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    Title :

    Method for calculation of heat transfer in laminar region of air flow around cylinders of arbitrary cross section (Including large temperature differences and transpiration cooling)


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1952


    Size :

    71 pages


    Remarks:

    Charts


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :