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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    Title :

    Streamline Curvature Design Procedure for Subsonic and Transonic Ducts


    Contributors:

    Publication date :

    1973


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English