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Advanced Composite Materials Volume 22, 2013 - Issue 4
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Articles

Thermal deformation constraint using response surfaces for optimization of stacking sequences of composite laminates

Akira Todoroki Department of Mechanical Sciences and Engineering, Tokyo Institute of Technology, 2-12-1 Ookayama, Meguro, Tokyo, 1528552, JapanCorrespondence[email protected]
,
Takumi Ozawa Department of Mechanical Sciences and Engineering, Tokyo Institute of Technology, 2-12-1 Ookayama, Meguro, Tokyo, 1528552, Japan
,
Yoshihiro Mizutani Department of Mechanical Sciences and Engineering, Tokyo Institute of Technology, 2-12-1 Ookayama, Meguro, Tokyo, 1528552, Japan
&
Yoshiro Suzuki Department of Mechanical Sciences and Engineering, Tokyo Institute of Technology, 2-12-1 Ookayama, Meguro, Tokyo, 1528552, Japan
Pages 265-279 | Received 13 Mar 2013, Accepted 13 May 2013, Published online: 04 Jun 2013

Citations (5)

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Read on this site (1)

Kazuhiro Sakata, Takashi Suzuki & Goichi Ben. (2018) Optimum structural design of CFRP isogrid cylindrical shell using genetic algorithm. Advanced Composite Materials 27:1, pages 35-51.
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Articles from other publishers (4)

Kanak Kalita, Salil Haldar & Shankar Chakraborty. (2022) A Comprehensive Review on High-Fidelity and Metamodel-Based Optimization of Composite Laminates. Archives of Computational Methods in Engineering 29:5, pages 3305-3340.
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Kanak Kalita, Shankar Chakraborty, S Madhu, Manickam Ramachandran & Xiao-Zhi Gao. (2021) Performance Analysis of Radial Basis Function Metamodels for Predictive Modelling of Laminated Composites. Materials 14:12, pages 3306.
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Kanak Kalita, Tanmoy Mukhopadhyay, Partha Dey & Salil Haldar. (2019) Genetic programming-assisted multi-scale optimization for multi-objective dynamic performance of laminated composites: the advantage of more elementary-level analyses. Neural Computing and Applications 32:12, pages 7969-7993.
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Akira Todoroki & Takumi Ozawa. (2013) Warping thermal deformation constraint for optimization of a blade stiffened composite panel using GA. International Journal of Aeronautical and Space Sciences 14:4, pages 334-340.
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