Application of Physics-Based Surrogate Models to Benchmark Aerodynamic Shape Optimization Problems
Author:
Affiliation:
1. Reykjavik University
2. Missouri University of Science and Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0265
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1. Hybrid feedback design for subsonic and transonic airfoils and wings
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