CFD Modeling of Separation and Transitional Flow in Low Pressure Turbine Blades at Low Reynolds Numbers
There is increasing interest in design methods and performance prediction for turbine engines operating at low Reynolds numbers. In this regime, boundary layer separation may be more likely to occur in the turbine flow passages. For accurate CFD predictions of the flow, correct modeling of laminar...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/29303 http://scholar.lib.vt.edu/theses/available/etd-10182009-105919/ |