Surface Modification Method for Aerodynamic Design Optimization
Author:
Affiliation:
1. Tohoku University, Sendai 980-8579, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.11181
Reference31 articles.
1. Lecture Series;Jameson A.,2003
2. Design optimization of high-lift configurations using a viscous continuous adjoint method
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5. Airfoil Design on Unstructured Grids for Turbulent Flows
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