Characterization of Flow Interactions in a One-Stage Shrouded Axial Turbine
The aim of this paper is to characterize the steady and unsteady flow interactions through a one-stage high-pressure (hp) shrouded axial turbine with a tip cavity. The vane and blade passages were reduced based on the scaling technique, and the domains of compromise were identified and used in the f...
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| 格式: | 文件 |
| 语言: | English |
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Wiley
2018-01-01
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| 丛编: | International Journal of Aerospace Engineering |
| 在线阅读: | http://dx.doi.org/10.1155/2018/3204859 |