Methods for calculating unit thermal conductance on outer surface of heated wing involving both laminar and turbulent boundary layers; new equation suggested should indicate effect of pressure gradient on laminar heat transfer to greater degree than heretofore; different equations applied to Joukowski profile.


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    Title :

    Investigation of aircraft heaters XXIX -- Comparison of several methods of calculating heat losses from airfoils


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    70 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    Investigation of Aircraft Heaters. 15 - The Emissivity of Several Materials

    L. M. Boelter / R. Bromberg / J. T. Gier | NTIS | 1944



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    Seidel, David A. / Batina, John T. / Whitlow, Woodrow, Jr. | NTRS | 1989