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 a design of a multicylinder engine for eventual flight applications.


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    Title :

    Lightweight Two-Stroke Cycle Aircraft Diesel Engine Technology Enablement Program. Volume 2


    Contributors:

    Publication date :

    1985


    Size :

    150 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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