Simultaneous Layout and Topology Optimization of Curved Stiffened Panels
Author:
Affiliation:
1. Cardiff University, Cardiff, Wales CF24 3AA, United Kingdom
2. University of California, San Diego, California 92093
Funder
Engineering and Physical Sciences Research Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060015
Reference39 articles.
1. Influence of stiffener location on the stability of stiffened plates under compression and in-plane bending
2. Preliminary design optimization of stiffened panels using approximate analysis models
3. Optimization methods for advanced design of aircraft panels: a comparison
4. Comparative Study on Optimal Stiffener Placement for Curvilinearly Stiffened Panels
5. EBF3PanelOpt: An optimization framework for curvilinear blade-stiffened panels
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