Algorithm and Turbulence Model Requirements for Simulating Vortical Flows
Author:
Affiliation:
1. University of Alabama
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-337
Reference44 articles.
1. High-Order-Accurate Methods for Complex Unsteady Subsonic Flows
2. Computational and Experimental Investigation of a Nonslender Delta Wing
3. 4Nichols.R.,Tramel,R.,andBuning,P."EvaluationofTwoHigherOrderWENOSchemes,"AIAA-2007-3920,Jun.2007.
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