Effect of Rotating Inlet Distortion with Multi-distorted Regions on Compressor Stability
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Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42405-024-00710-y.pdf
Reference19 articles.
1. Li J, Dong X, Sun D, Xu R, Sun X (2021) Response and stabilization of a two-stage axial flow compressor restricted by rotating inlet distortion. Chin J Aeronaut 34(9):72–82. https://doi.org/10.1016/j.cja.2021.02.005
2. Lee K-B, Wilson M, Vahdati M (2018) Effects of inlet disturbances on fan stability. J Eng Gas Turbines Power 141(5):051014. https://doi.org/10.1115/1.4042204
3. Longley JP, Shin H-W, Plumley RE, Silkowski PD, Day IJ, Greitzer EM, Tan CS, Wisler DC (1996) Effects of rotating inlet distortion on multistage compressor stability. J Turbomach 118(2):181–188. https://asmedigitalcollection.asme.org/turbomachinery/article-pdf/118/2/181/5501129/181_1.pdf. https://doi.org/10.1115/1.2836624
4. Ludwig GR, Arendt RH, Nenni JP (1973) Investigation of rotating stall in axial flow compressors and the development of a prototype stall control system, Usaf-apl-tr-73-45 edn. USAF
5. Peters T, Fottner L (2002) Effects of co- and counter-rotating inlet distortions on a 5-stage HP-compressor. Turbo expo: power for land, sea, and air, vol 5: Turbo Expo 2002, Parts A and B, pp 659–666. https://doi.org/10.1115/GT2002-30395
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