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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    Titel :

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


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Boelter, L.M.K. (Autor:in) / Grossman, L.M. (Autor:in) / Martinelli, R.C. (Autor:in) / Morrin, E.H. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    70 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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

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



    Calculating Transonic Flows About Airfoils

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