Numerical simulations of surge and rotating-stall in multi-stage axial-flow compressors-Reference-Cited by-同舟云学术

Numerical simulations of surge and rotating-stall in multi-stage axial-flow compressors

Published:1994-06-27 Issue: Volume: Page:
ISSN:
Container-title:30th Joint Propulsion Conference and Exhibit
language:
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Author:

Escuret J.¹,Garnier V.¹

Affiliation:

1. SNECMA, Moissy-Cramayel, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3202

Reference18 articles.

1. [I] Day, I.J., Freeman, C., 1993, "The Unstable BehavionrofLowandHigh SpeedCompressors", ASME Papcr: 93-GT-26 121 Wilson, A., Freeman, C., 1993,"StallInception andDevelopmentin an AxialFlowAeroengine",ASME Paper 93-GT-2

2. Davis, M.W., O'Brien, W.F., 1987, "A Stageby-stage Post-stall Compression System Modeling Technique", AIAAPaper: AIAA-87-2088

3. Escuret,J.F., Elder,RL., 1993,"ActiveControl of Surge in Multi-stage Axial-flow Compressors", ASMEPaper 93-GT-39

4. A Theory of Post-Stall Transients in Axial Compression Systems: Part I—Development of Equations

5. Longley, J.P., 1993, "A Review of Non-steady Flow Models for Compressor Stability", ASME Paper: 93-GT-17

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