Lightweight design of cylindrical stiffened shells in launch vehicles by a dual-elite population sequential approximation optimization approach-Reference-Cited by-同舟云学术

Lightweight design of cylindrical stiffened shells in launch vehicles by a dual-elite population sequential approximation optimization approach

Published:2020-06-09 Issue:6 Volume:53 Page:984-1004
ISSN:0305-215X
Container-title:Engineering Optimization
language:en
Short-container-title:Engineering Optimization

Author:

Wang Zhixiang¹,Lei Yongjun¹,Wu Zeping¹,OuYang Xing²,Zhang Dapeng¹,Liu Guanri²

Affiliation:

1. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, People’s Republic of China

2. Beijing Institute of Astronautical Systems Engineering, Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

National University of Defense Technology

Publisher

Informa UK Limited

Subject

Applied Mathematics,Industrial and Manufacturing Engineering,Management Science and Operations Research,Control and Optimization,Computer Science Applications

Link

https://www.tandfonline.com/doi/pdf/10.1080/0305215X.2020.1767097

Reference48 articles.

1. Post-buckling and collapse experiments of stiffened composite cylindrical shells subjected to axial loading and torque

2. Post-buckling optimisation of composite stiffened panels using neural networks

3. Determination of realistic worst imperfection for cylindrical shells using surrogate model

4. Nonlinear equilibrium of imperfect, locally deformed stringer-stiffened panels under combined in-plane loads

5. Numerical–experimental investigation on post-buckled stiffened composite panels

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