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- W3148558412 abstract "The stall mechanism of the NASA Rotor 37 is investigated through the analysis of the critical flow structures near the stall under the transonic condition. The performance of the rotor with Circumferential Grooves Casing Treatment (CGCT) is also studied based on the Reynolds-Averaging Navier-Stokes approach. The study finds that stall margin improvement can be achieved without significant penalty on the efficiency for the two CGCT configurations applied. The effects of circumferential grooves on the critical flow structures are studied through the analysis of the tip leakage mass and momentum transport that further re-veal the CGCT mechanism." @default.
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- W3148558412 date "2010-01-01" @default.
- W3148558412 modified "2023-09-23" @default.
- W3148558412 title "An analysis of the Circumferential Grooves Casing Treatment for transonic compressor flow" @default.
- W3148558412 hasPublicationYear "2010" @default.
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