Hybrid Slot-Groove Casing Treatment for Stall Margin Improvement on an Axial Flow Compressor with Circumferential Total Pressure Distortion
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s11630-023-1750-x.pdf
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4. Fidalgo V.J., Hall C.A., Colin Y., A study of fan-distortion interaction within the NASA rotor 67 transonic stage. Journal of Turbomachinery, 2012, 134(5): 051011.
5. Dong X., Sun D., Li F., Sun X., Stall margin enhancement of a novel casing treatment subjected to circumferential pressure distortion. Aerospace Science and Technology, 2018, 73: 239–255.
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1. The influence of a coupled casing on the performance of a multistage compressor under inlet distortion conditions;AIP Advances;2023-12-01
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