A procedure for designing ducts for subsonic and transonic speeds is described. Examples discussed are a wind-tunnel contraction cone, a supersonic nozzle, and a diffuser. A listing of the computer program is included. The streamline curvature equations represent a form of the exact, compressible, inviscid flow equations. The method is applicable from low subsonic to supersonic speeds. (Author)


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    Titel :

    Streamline Curvature Design Procedure for Subsonic and Transonic Ducts


    Beteiligte:
    R. L. Barger (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch