Influence of nose forms, skirts, flaps, propellers, spinners, and special blowers investigated; results show comparative inefficiency of adjustable skirt flaps, detrimental effect of small-diameter front openings of cowling, and beneficial effect of carefully designed airfoil section near hub of propeller.


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    Titel :

    Cooling of airplane engines at low air speeds


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Theodorsen, T. (Autor:in) / Brevoort, M.J. (Autor:in) / Stickle, G. (Autor:in)


    Erscheinungsdatum :

    1937


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Cooling of airplane engines at low air speeds

    Theodorsen, T. / Brevoort, M.J. / Stickle, G.W. | Engineering Index Backfile | 1937


    Cooling of Airplane Engines at Low Air Speeds

    Theodorsen, Theodore / Brevoort, M J / Stickle, George W | NTRS | 1937


    Cooling of airplane engines at low air speeds

    Theodorsen, T. / Brevoort, M.J. / Stickle, G.W. | Engineering Index Backfile | 1937


    Torsional critical speeds of geared airplane engines

    Den Hartog, J.P. / Butterfield, J.P. | Engineering Index Backfile | 1937


    Coolings of airplane engines at low air speeds

    Theodorsen, Theodor / Brevoort, M. J. / Stickle, George W. | TIBKAT | 1937