Optimization of a Prop-Fan propulsion system for a Mach 0.8, 120 passenger commercial transport has shown the need for relatively high levels of overall pressure ratio, combustor exit temperature, propeller tip speed and propeller disk loading to achieve lowest fuel burn and direct operating costs. Comparison of this optimized Prop-Fan propulsion system with an equivalent technology turbofan showed it to have significant mission fuel burn and direct operating cost advantages.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Some Aspects of Prop-Fan Propulsion Systems Analysis


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Aerospace Congress and Exposition ; 1982



    Erscheinungsdatum :

    1982-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Prop-Fan Propulsion -Its Status and Potential

    Gatzen, Bernard S. / Dugan, James F. / Adamson, William M. | SAE Technical Papers | 1978


    Prop-fan propulsion - Its status and potential

    Dugan, J. F., Jr. / Gatzen, B. S. / Adamson, W. M. | NTRS | 1978


    Prop-Fan propulsion - Its status and potential

    Dugan, J.F. jun. / Gatzen, B.S. / Adamson, W.M. | Tema Archiv | 1978



    Some aspects of underwater jet propulsion systems

    Gongwer, C.A. | Engineering Index Backfile | 1961