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    Streamline curvature design procedure for subsonic and transonic ducts (1973)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: 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.
    Keywords: AERODYNAMICS
    Type: NASA-TN-D-7368 , L-8963
    Format: application/pdf
    Location Call Number Expected Availability
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