Wing Optimization Using Design of Experiment, Response Surface, and Data Fusion Methods
- 1 July 2003
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 40 (4), 741-750
- https://doi.org/10.2514/2.3153
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Concise Orthogonal Representation of Supercritical AirfoilsJournal of Aircraft, 2001
- Two-level composite wing structural optimization using response surfacesStructural and Multidisciplinary Optimization, 2000
- Aircraft wing design using GA-based multi-level strategiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- A trust-region framework for managing the use of approximation models in optimizationStructural and Multidisciplinary Optimization, 1998
- Variable-complexity aerodynamic optimization of a high-speed civil transport wingJournal of Aircraft, 1994
- A Fast Genetic Algorithm with Sharing Scheme Using Cluster Analysis Methods in Multimodal Function OptimizationPublished by Springer Science and Business Media LLC ,1993
- Accurate prediction of drag using Euler methodsJournal of Aircraft, 1992
- Comparison of Three Methods for Selecting Values of Input Variables in the Analysis of Output from a Computer CodeTechnometrics, 1979
- A Simplex Method for Function MinimizationThe Computer Journal, 1965
- An Automatic Method for Finding the Greatest or Least Value of a FunctionThe Computer Journal, 1960