Tests in full-scale wind tunnel on mock-up of YO-31A airplane to determine drag of Prestone and oil radiators exposed on lower surface of fuselage; at 120 mph oil radiator accounted for 2.8% of drag of complete airplane, Prestone radiator, for 8.3%; and both radiators together for 11.8%.


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    Titel :

    Drag of prestone and oil radiators on YO-31A Airplane


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    DeFrance, S.J. (Autor:in)


    Erscheinungsdatum :

    1935


    Format / Umfang :

    3 pages


    Anmerkungen:

    5 Supp Sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Tests of airplane radiators

    Heldt, P.M. | Engineering Index Backfile | 1919


    DESIGN FACTORS FOR AIRPLANE RADIATORS

    PARSONS, SAMUEL R | SAE Technical Papers | 1920


    Design factors for airplane radiators

    Parsons, Samuel R. | Engineering Index Backfile | 1920