The technology that will improve the energy efficiency of propulsion systems for subsonic commercial aircraft is investigated. A reduction of 14.4% in cruise installed sfc (0.572 versus 0.668 for the CF6-50C) and a direct operation cost reduction in excess of the 5% goal is projected. Noise and emissions projections are consistent with the established goals.


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    Title :

    Energy efficient engine component development and integration program


    Publication date :

    1981-01-30


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English