Computational Simulations of Compressible Transitional Flows in a Turbine Vane Cascade
In order to improve the efficiency and reduce the emissions of aircraft engines, new combustor designs have been developed to reduce outlet temperatures and increase mixing. At high altitudes, the low pressure and low Reynolds number flow would normally produce a laminar boundary layer on the turbi...
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| Format: | Others |
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North Dakota State University
2019
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| Online Access: | https://hdl.handle.net/10365/29783 |