Zonal detached-eddy simulation applied to the tip-clearance flow in an axial compressor

被引:0
|
作者
Riéra, W. [1 ]
Marty, J. [1 ]
Castillon, L. [1 ]
Deck, S. [1 ]
机构
[1] ONERA-The French Aerospace Lab, 8 rue des Vertugadins, Meudon,92190, France
来源
Journal of Aircraft | 2016年 / 53卷 / 04期
关键词
Flow separation - Spectrum analysis - Wakes - Leakage (fluid) - Unsteady flow - Navier Stokes equations - Axial flow turbomachinery;
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页码:2377 / 2391
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