Propulsion System Flow Stability Program (Dynamic). Part IX. Model for Predicting Compressor Performance with Combined Circumferential and Radial Distortion - Computed and Experimental Results.
Final technical rept. 20 Jun 67-30 Sep 68 on Phase 1,
NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV
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This report presents the computed results obtained with a computer program designed to predict the performance of a multistage axial compressor operating with combined circumferential and radial distortion it presents comparisons between the computed performance and that experimentally realized on a number of compressor configurations. Author
- Fluid Mechanics
- Jet and Gas Turbine Engines