A Time-Accurate CFD Analysis of Inlet Distortion Induced Swirl in Multistage Fans
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American Institute of Aeronautics and Astronautics
Reference20 articles.
1. 1Langston, C. “Distortion Tolerance - By Design Instead of By Accident,” ASME Paper 69-GT-115, ASME, 1969.
2. Multiple Segment Parallel Compressor Model for Circumferential Flow Distortion
3. 4Reid, C. “The Response of Axial Flow Compressors to Intake Flow Distortion,” ASME Paper 69-GT-29, ASME, 1969.
4. 5Plourde, G. and Stenning, A. “The Attenuation of Circumferential Inlet Distortion In Multi-Stage Axial Compressors,” AIAA Paper 67-415, AIAA 3rd Propulsion Joint Specialist Conference, Washington, D.C., July 1967.
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