Gappy Proper Orthogonal Decomposition-Based Two-Step Optimization for Airfoil Design
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050997
Reference18 articles.
1. Optimal design of two-dimensional wings in ground effect using multi-objective genetic algorithm
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5. Hybrid method for aerodynamic shape optimization in automotive industry
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