An unsteady numerical analysis of a generic non-axisymmetric turbine endwall in a 11/2 stage turbine test rig

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Department of Mechanical and Mechatronic Engineering, University of Stellenbosch, Pretoria, South Africa [1 ]
不详 [2 ]
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Aeronaut J | / 1211卷 / 109-119期
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10.1017/s0001924000010277
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