Wing Optimization Using Design of Experiment, Response Surface, and Data Fusion Methods
Author:
Affiliation:
1. University of Southampton, Highfield, Southampton, England SO17 1BJ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3153
Reference25 articles.
1. Aircraft wing design using GA-based multi-level strategies
2. Concise Orthogonal Representation of Supercritical Airfoils
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