Comparison of approximation models with merit functions for design optimization
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-4754
Reference17 articles.
1. Thomas A. Zang and Lawrence L. Green. "Multidisciplinary Design Optimization Techniques: Implications and Opportunities for Fluid Dynamics," 30th AIAA Fluid Dynamics Conference, Norfolk, Viginia, AIAA99-3798,June 1999
2. 2Jaroslaw Sobieszczanski-Sobieski and Raphael T. Haftka "Multidisciplinary Aerospace Design Optimization: Survey of Recent Developments," 34th AIAA Aerospace Sciences Meeting and Exhibit , Reno, Nevada, AIAA96-0711,January 1996.
3. 3Resit Unal, Roger A. Lepsch, Jr. and Mark L. McMillin "Response Surface Model Building and Multidisciplinary Optimization Using Overdetermined D-Optimal Designs," 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, St. Louis, Missouri, AIAA98-4759,September 1998
4. 4Anthony A. Giunta and Layne T. Watson "A Comparison of Approximation Modeling Techniques: Polynomial Versus Interpolating Models," 7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization , St. Louis, Missouri, AIAA98-4758,September 1998.
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