Aeroelastic Topology Optimization of Blade-Stiffened Panels
Author:
Affiliation:
1. Universal Technology Corporation, U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032500
Reference27 articles.
1. Analysis and Limit State Design of Stiffened Plates and Shells: A World View
2. Comparative Study on Optimal Stiffener Placement for Curvilinearly Stiffened Panels
3. Multiobjective Evolutionary Structural Optimization Using Combined Static/Dynamic Control Parameters
4. A systematic topology optimization approach for optimal stiffener design
5. Automated rib location and optimization for plate structures
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