Supersonic throughflow fan research, and technology needs are reviewed. The design of a supersonic throughflow fan stage, a facility inlet, and a downstream diffuser is described. The results from the analysis codes used in executing the design are shown. An engine concept intended to permit establishing supersonic throughflow within the fan on the runway and maintaining the supersonic throughflow condition within the fan throughout the flight envelope is presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Supersonic Throughflow Fans


    Beteiligte:
    C. L. Ball (Autor:in) / R. D. Moore (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Supersonic throughflow fans

    Ball, C. L. / Moore, R. D. | NTRS | 1988


    Supersonic throughflow fans for high-speed aircraft

    Ball, Calvin L. / Moore, Royce D. | NTRS | 1990




    Supersonic Throughflow Fans for High-Speed Aircraft

    C. L. Ball / R. D. Moore | NTIS | 1990