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)
Streamline Curvature Design Procedure for Subsonic and Transonic Ducts
1973
18 pages
Report
No indication
English
An improved streamline curvature approach for transonic axial compressor performance prediction
Online Contents | 2011
|An improved streamline curvature approach for transonic axial compressor performance prediction
SAGE Publications | 2011
|