Aerodynamic Loss Sources in Axial-Flow Compressors.
Final rept. 6 Jan 83-31 Aug 86,
IOWA STATE UNIV AMES ENGINEERING RESEARCH INST
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Research related to understanding and modeling aerodynamic loss production in axial-flow compressors was accomplished. Some progress in clarification of loss prediction was attained. Suggestions for incorporating wake interaction effects in axial-flow compressor design calculations are offered. Some of the inherent complications associated with supersonic blade testing are noted. Further study of specific details of loss generation is proposed. Keywords Axial-flow turbomachinery Turbomachine flow measurement Computational fluid mechanics.
- Jet and Gas Turbine Engines