Lightweight design of cylindrical stiffened shells in launch vehicles by a dual-elite population sequential approximation optimization approach. Issue 6 (3rd June 2021)

• Record Type: Journal Article
• Authors: Wang, Zhixiang; Lei, Yongjun; Wu, Zeping; OuYang, Xing; Zhang, Dapeng; Liu, Guanri
• Is Part Of: Engineering optimization. Volume 53:Issue 6(2021)
• Page Start: 984
• Page End: 1004
• Publication Date: 2021-06-03
• Subjects: Cylindrical stiffened shells -- postbuckling -- sequential approximation optimization -- dual-elite population -- adaptive parallel infilling strategy; Engineering design -- Periodicals; Mathematical optimization -- Periodicals; 620.0042
• DOI: 10.1080/0305215X.2020.1767097
• Languages: English
• ISSNs: 0305-215X

Abstract

Abstract : A nonlinear displacement-controlled loading dynamic method is employed to investigate the deformed shape evolution of stiffened shells from prebuckling to postbuckling field until collapse. Because of the time-consuming postbuckling analysis, the dual-elite population sequential approximation optimization (SAO) approach is proposed. A novel determination method of Gaussian kernel widths based on moment estimates is proposed to enhance the augmented radial basis function surrogate model. A novel adaptive parallel infilling strategy is then developed to balance the capabilities of local and global optimization. A dual-elite population strategy is further developed to exploit the information from already acquired sampling points. Finally, the framework of the proposed SAO approach, which is implemented in a distributed parallel way on high-performance clusters to further diminish computation costs, is presented. The efficiency of the algorithm is validated by the postbuckling lightweight optimization of a cylindrical stiffened shell, resulting in a reduction of 12.3% of the initial weight.