An experimental Single Cylinder Test Engine Program is conducted to confirm the analytically projected performance of a two-stroke cycle diesel engine for aircraft applications. Testing confirms the ability of a proposed 4-cylinder version of such an engine to reach the target power at altitude in a highly turbocharged configuration. The experimental program defines all necessary parameters to permit design of a multicylinder engine for eventual flight applications.


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    Titel :

    Lightweight Two-Stroke Cycle Aircraft Diesel Engine Technology Enablement Program. Volume 3


    Beteiligte:
    P. D. Freen (Autor:in) / S. G. Berenyi (Autor:in) / A. P. Brouwers (Autor:in) / M. E. Moynihan (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    282 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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