Results of investigation of large chord wing model with duct to house simulated radiator suitable for liquid cooled engine; duct was expanded to reduce radiator losses, and installation of duct and radiator was made entirely within wing to reduce form and interference drag.


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    Titel :

    Investigation in 7- by 10-foot wind tunnel of ducts for cooling radiators within airplane wing


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Harris, T.A. (Autor:in) / Recant, I.G. (Autor:in)


    Erscheinungsdatum :

    1942


    Format / Umfang :

    19 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Nelson, W.J. / Czarnecki, K.R. | Engineering Index Backfile | 1943





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