Variable-complexity response surface approximations for wing structural weight in HSCT design
Author:
Affiliation:
1. Virginia Polytechnic Inst. and State Univ., Blacksburg
2. Florida, Univ., Gainesville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-89
Reference25 articles.
1. Variable-complexity aerodynamic optimization of a high-speed civil transport wing
2. Variable-complexity aerodynamic-structural design of a high-speed civil transport wing
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