Multifidelity Physics-Based Method for Robust Optimization Applied to a Hovering Rotor Airfoil
Author:
Affiliation:
1. Department of Aerospace Science and Technology, Politecnico di Milano, 20156 Milan, Italy
2. Bordeaux–Sud-Ouest Centre, Institut National de Recherche en Informatique et en Automatique, 33405 Talence Cedex, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053952
Reference54 articles.
1. Wing Design by Numerical Optimization
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4. Aerodynamic shape optimization techniques based on control theory
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