The response of a low speed compressor on rotating inlet distortion
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-006-0314-2.pdf
Reference4 articles.
1. Hynes, T.P. and Greitzer, E.M. A Method for Assessing Effects of Inlet Flow Distortion on Compressor Stability. ASME J. Turbomachinery 1987, Vol. 109, pp 371–379
2. J.P. Longley et al. Effects of Rotating Inlet Distortion on Multistage Compressor Stability. ASME 94-GT-220. 1994
3. Thomas Peters et al. Effects of Rotating Inlet Distortion on a 5-Stage HP-Compressor. ASME 2001-GT-0300, 2001
4. Reid C. The Response of Axial Flow Compressors to Intake Flow Distortion. ASME 69-GT-29. 1969
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