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Propulsion System Flow Stability Program (Dynamic). Part VIII. Model for Predicting Compressor Performance with Combined Circumferential and Radial Distortion - Computer Program.Author(s): Novak, R. A., Hearsey, R. M.
Corporate Author(s): Northern Research and Engineering Corporation
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1968-12
Report number: AFAPL TR 68-142 Part VIII