Optimal Design of Composite Wing Structures with Blended Laminates
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4349
Reference13 articles.
1. Ragon, S., Gürdal, Z., Hafka, R. T., and Tzong, T. J. "Global/Local Structural Wing Design Using Response Surface Techniques", Proceedings of the 38thAIAA / ASME / ASCE / AHS / ASC Structures, Structural Dynamics and Materials Conference, Kissimmee, FL, April7-10,1997, 1204-1214.
2. Composite wing structural optimization using genetic algorithms and response surfaces
3. Two-level composite wing structural optimization using response surfaces
4. Liu, B., and Hafka, R. T. "Composite Wing Structural Design Optimization with Continuity Constraints", Proceedings of the 42ndAIAA/ASME/ASCE/AHS/ASCStructures,StructuralDynamicsandMaterialsConference,Seattle,WA,April16-19, 2001.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Optimal design of composite wing structures with blended laminates;Composites Part B: Engineering;2007-06
2. Global/Local Iteration for Blended Composite Laminate Panel Structure Optimization Subproblems;Mechanics of Advanced Materials and Structures;2007-04
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