Effect of rotor blade tip clearance on aerodynamic performance of high-speed multi-stage axial compressor
Using a high-speed multistage scale model compressor simulating a middle stage of a gas turbine compressor for power generation, the effects of 3 types of rotor tip clearances on performance and operating range, and the vortex structure of rotor tip leakage vortices were investigated numerically and...
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| Format: | Article |
| Language: | Japanese |
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The Japan Society of Mechanical Engineers
2023-12-01
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| Series: | Nihon Kikai Gakkai ronbunshu |
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| Online Access: | https://www.jstage.jst.go.jp/article/transjsme/90/929/90_23-00207/_pdf/-char/en |