A novel sensitivity analysis method for high fidelity multidisciplinary optimization of aero-structural systems
Author:
Affiliation:
1. NRC/NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-683
Reference33 articles.
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3. Supersonic transport wing minimum weight design integrating aerodynamics and structures
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