Stall inception prediction of axial compressors with radial inlet distortions
Author:
Funder
National Science and Technology Major Project
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference42 articles.
1. Effects of rotating inlet distortion on multistage compressor stability;Longley;ASME J. Turbomach.,1996
2. Effects of rotating inlet distortion on a 5-stage HP-compressor;Peters,2001
3. The influence of inlet swirl distortions on the performance of a jet propulsion two-stage axial compressor;Pazur;ASME J. Turbomach.,1991
4. Steady performance measurements of a turbofan engine with inlet distortions containing co- and counter rotating swirl from an intake diffuser for hypersonic flight;Schmid;ASME J. Turbomach.,2001
5. Compressor performance and operability in swirl distortion;Sheoran;ASME J. Turbomach.,2012
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