Description of tests made with Curtiss plant Model P-6 which was first pursuit plane built to incorporate engine high-temperature liquid cooling feature; improvements in airplane structure allowed by new engine cooling system; series of tests started with ethylene glycol; advantages in greater fuel economy and reduced radiator size.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    An improved cooling system for aircraft engines


    Weitere Titelangaben:

    Air Corps News Letter


    Beteiligte:
    Jacobs, A.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1929


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Liquid cooling of aircraft engines

    Weidinger, H. | Engineering Index Backfile | 1931


    Liquid cooling of aircraft engines

    Weidinger, H. | Engineering Index Backfile | 1931


    Liquid cooling of aircraft engines

    Weidinger, Hanns | TIBKAT | 1931


    The evaporative cooling of aircraft engines

    Cave-Browne-Cave, T.R. | Engineering Index Backfile | 1925


    High - Conductivity Cooling Fins for Aircraft Engines

    CUNNINGHAM, J. W. | SAE Technical Papers | 1945