A brief overview is provided of past supersonic throughflow fan activities; technology needs are discussed; the design is described of a supersonic throughflow fan stage, a facility inlet, and a downstream diffuser; and the results are presented from the analysis codes used in executing the design. Also presented is a unique 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.


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    Titel :

    Supersonic Throughflow Fans for High-Speed Aircraft


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

    Erscheinungsdatum :

    1990


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Supersonic throughflow fans for high-speed aircraft

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




    Supersonic Throughflow Fans

    C. L. Ball / R. D. Moore | NTIS | 1988


    Supersonic throughflow fans

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