Geometric Filtration Using Proper Orthogonal Decomposition for Aerodynamic Design Optimization
Author:
Affiliation:
1. University of Southampton, Southampton, England SO17 1BJ, United Kingdom
2. Airbus Operations Ltd., Bristol, England BS99 7AR, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.41420
Reference39 articles.
1. Optimized Nonuniform Rational B-Spline Geometrical Representation for Aerodynamic Design of Wings
2. A Study of Shape Parameterisation Methods for Airfoil Optimisation
3. Airfoil Shape Optimization Using a Nonuniform Rational B-Splines Parametrization Under Thickness Constraint
4. Wing Design by Numerical Optimization
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