Modern high output aircraft engine and requirement to fly it at altitudes beyond 30,000 ft has introduced problems in aircraft oil system; factors are reviewed from standpoint of their effect on pump performance at high altitudes. Illustrations not included with mimeographed copy. (Trans)


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    Titel :

    Aircraft oil systems -- High-altitude problems


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Moerman, H.E. (Autor:in)


    Erscheinungsdatum :

    1943


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    AIRCRAFT OIL SYSTEMS HIGH - ALTITUDE PROBLEMS

    MOERMAN, H. E. | SAE Technical Papers | 1943


    OZONE PROBLEMS IN HIGH ALTITUDE AIRCRAFT

    SAE Technical Papers | 1965


    OZONE PROBLEMS IN HIGH ALTITUDE AIRCRAFT

    SAE Technical Papers | 1996


    High-Altitude Aircraft Oil Systems

    Carroll, F.E. | SAE Technical Papers | 1950


    High-Altitude Aircraft Platform-M55 Geophysica High-Altitude Research M55 Aircraft

    Sokolov, L. A. | British Library Conference Proceedings | 1997