Effects of Non-uniform Inlet Flow on the Flow Stability of a Transonic Compressor Rotor
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-16-8154-7_21
Reference10 articles.
1. Chen H (2020) Investigation of compressor flow instabilities based on global linear stability analysis. Beihang University, Beijing
2. Hah C, Rabe DC, Sullivan TJ, Wadia AR (1998) Effects of inlet distortion on the flow field in a transonic compressor rotor. ASME J Turbomach 120(2):233–246
3. Spakovszky ZS, Weigl HJ, Paduano JD, van Schalkwyk CM, Suder KL, Bright MM (1999) Rotating stall control in a high-speed stage with inlet distortion: part i—radial distortion. ASME J Turbomach 121(3):510–516
4. Ferrand P, Chauvin J (1982) Theoretical study of flow instabilities and inlet distortions in axial compressors. ASME J Eng Power 104(3):715–721
5. Yao J, Gorrell SE, Wadia AR (2010) High-fidelity numerical analysis of per-rev-type inlet distortion transfer in multistage fans—part i: simulations with selected blade rows. ASME J Turbomach 132(4):041014
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