Performance Analysis of Inter-Stage Leakage Flows at Rotating Conditions in an Axial Compressor
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s11630-020-1378-z.pdf
Reference20 articles.
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3. Yoon S., Selmeier R., Cargill P., Peter W., Effects of the stator hub configuration and stage design parameters on aerodynamic loss in axial compressors. Journal of Turbomachinery, 2015, 137(9): 091001.
4. Kong X.Z., Liu G.W., Liu Y.X., Zheng L.X., Experimental testing for the influences of rotation and tip clearance on the labyrinth seal in a compressor stator well. Aerospace Science and Technology, 2017, 71(12): 556–567.
5. Li J., Yan X., Li G.J., Feng Z.P., Effects of pressure ratio and sealing clearance on leakage flow characteristics in the rotating honeycomb labyrinth seal. ASME Turbo Expo 2007: Power for Land, Sea, and Air, Montreal, Canada, 2007, Paper No. GT2007-27740. DOI: https://doi.org/10.1115/GT2007-27740.
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