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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Energy Efficient Engine Component Development and Integration Program


    Erscheinungsdatum :

    1981


    Format / Umfang :

    412 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch