Multifidelity response surface model for HSCT wing bending material weight
Author:
Affiliation:
1. Vanderplaats Research and Development, Inc., Colorado Springs, CO
2. Virginia Polytechnic Inst. and State Univ., Blacksburg
3. Florida, Univ., Gainesville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-4804
Reference19 articles.
1. Multidisciplinary aerospace design optimization: survey of recent developments
2. Variable-Complexity Multidisciplinary Design Optimization Using Parallel Computers
3. Variable-complexity response surface approximations for wing structural weight in HSCT design
4. HSCT configuration design using response surface approximations of supersonic Euler aerodynamics
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