High speed centrifugal compressor surge initiation characterization-Reference-Cited by-同舟云学术

High speed centrifugal compressor surge initiation characterization

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
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Author:

Oakes William¹,Lawless Patrick¹,Fagan John¹,Fleeter Sanford¹

Affiliation:

1. Purdue Univ., West Lafayette, IN

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2577

Reference17 articles.

1. Haupt, U., Abdel-Hamid, A.N., Kaemmer, N. and Rautenber, M, 1986, "Excitation of Blade Vibration by Flow Instability in Centrifugal Compressors", ASMEPaper 86-GT-283.

2. Hin, D., Haupt, U., Hasenmann, H., and Rautenberg, M, 1992, "Blade Excitation by Circumferentially Asymmetric Rotating Stall in Centrifugal Compressors", ASME Paper 92-GT148.

3. Stall Inception in Axial Flow Compressors

4. McDougall, N.M., Cumpsty, N.A. and Hynes, T.P., 1990, "Stall Inception in Axial Compressors,* Journal of Turbomachinery, Vol. 112,No. 1,January,pp. 116-125.

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