Composite wing structural design optimization with continuity constraints
Author:
Affiliation:
1. Florida, Univ., Gainesville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1205
Reference3 articles.
1. Two-level composite wing structural optimization using response surfaces
2. Global/local structural wing design using response surface techniques
3. Schmit, L.A.,and Mehrinfar, M."Multilevel Optimum Design of Structures with Fiber-Composite Stiffened Panel Components", 4/44./., 20(1),1982,pp.138-147.
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