Study of Transitional Flow Through a Low-Pressure Turbine Cascade by Application of Higher-Order Compact-Difference Scheme to Large-Eddy Simulation-Reference-Cited by-同舟云学术

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Study of Transitional Flow Through a Low-Pressure Turbine Cascade by Application of Higher-Order Compact-Difference Scheme to Large-Eddy Simulation

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Fluid Dynamics Conference and Exhibit
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Author:

Poondru Shirdish¹,Ghia Urmila¹,Ghia Karman¹

Affiliation:

1. University of Cincinnati

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2882

Reference20 articles.

1. Experimental Study of the Unsteady Aerodynamics in a Linear Cascade With Low Reynolds Number Low Pressure Turbine Blades

2. 2Suzen, Y. B, Huang, P. G., Volino, R. J. etal (2003) "A Comprehensive CFD Study of Transitional Flows in Low-PressureTurbinesUnder aWideRange ofOperatingConditions,"AIAA Paper2003-3591.June2003.

3. High-Resolution Large-Eddy Simulation of Flow Around Low-Pressure Turbine Blade

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