Mesh generation for turbomachinery blade passages with three dimensional endwall features
Turbomachinery blade passages are conventionally meshed by sweeping a mesh from a reference stream surface to other stream surfaces along the blade span. This approach is widely used in the gas turbine industry but it becomes problematic for simulations where the flow close to the endwall region is...
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| Format: | Journal article |
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American Institute of Aeronautics and Astronautics
2017
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