Tip air injection to extend stall margin of multi-stage axial flow compressor with inlet radial distortion
Author:
Funder
National Science Foundation of China
Youth Innovation Promotion Association
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference43 articles.
1. Stall, surge, and 75 years of research;Day;J. Turbomach.,2016
2. Viscous throughflow modeling for multistage compressor design;Howard;J. Turbomach.,1993
3. Development and application of a multistage Navier–Stokes flow solver: part II—application to a high-pressure compressor design;LeJambre;J. Turbomach.,1998
4. Secondary flows, endwall effects, and stall detection in axial compressor design;Banjac;J. Turbomach.,2015
5. A design strategy for a 6:1 supersonic mixed-flow compressor stage;Sadagopan;Aerosp. Sci. Technol.,2019
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