Determining chordwise distribution of rate of heat transfer from surface of wing or body of revolution to air with view to ice prevention on aircraft; comparison of calculated average heat transfer coefficient for nose section of wing of Lockheed 12-A airplane with that experimentally determined shows satisfactory agreement. (25¢)


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    Title :

    Method for calculating heat transfer in laminar flow region of bodies


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Allen, H.J. (author) / Look, B.C. (author)


    Publication date :

    1947


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :