A Comparison of Two POD Methods for Airfoil Design Optimization
Author:
Affiliation:
1. Thaerocomp Technical Corporation
2. State University of New York at Stony Brook
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4912
Reference24 articles.
1. Jameson,A."AdvancesinAerodynamicShapeOptimization,"InternationalConferenceonCFD,Toronto,Canada,12-16 July, 2004.
2. 3Romanowski,M.C."ReducedOrderUnsteadyAerodynamicandAeroelasticModelsUsingKarhunen-Loève Eigenmodes," AIAA-96-3981,1996.
3. 4Glauser,M.N.,etal."PODBasedExperimentalFlowControlonaNACA-4412Airfoil(Invited),"AIAA-2004-0575.
4. Reduced-order modeling: new approaches for computational physics
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