Theoretical and experimental validation of the variable-thickness topology optimization approach for the rib-stiffened panels

被引:2
|
作者
Ko, Kyaw Ye [1 ]
Solyaev, Yury [1 ]
Lurie, Sergey [1 ]
Babaytsev, Arseniy [1 ]
Rabinskiy, Lev [1 ]
Kondakov, Ivan [2 ]
机构
[1] Moscow Inst Aviat Technol, Volokolamskoe Ave 4, Moscow 125993, Russia
[2] Cent Aerohydrodynam Inst, Zhukovskiy Str 1, Zhukovskii 140180, Russia
关键词
Topology optimization; Rib-stiffened plates; Variable thickness; Compliance minimization; Gradient constraint; Experimental validation; THIN ELASTIC PLATES; OPTIMAL-DESIGN; LAYOUT;
D O I
10.1007/s00161-023-01224-w
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this paper, we consider compliance minimization problems within the variable-thickness approach for the rib-stiffened plates subjected to a transverse loading. It is known, that such optimization problems are usually not well posed and their solutions become strongly mesh-dependent. To overcome this issue, we introduce additional regularization constraint on the thickness gradient and evaluate the convergence and efficiency of considered method. Variable thickness is defined based on topology optimization approach introducing additional design variables in the nodes of the shell-type elements. Numerical solutions are provided by using finite element simulations within Mindlin-Reissner theory and method of moving asymptotes. Possibility for the well-converged optimal solutions for the benchmark problems with rib-stiffened panels loaded by the systems of concentrated forces is shown. Parametric studies are provided to analyse the effects of the shape functions order, values of penalty factors and initial conditions for the plate thickness. Recommendations for the optimal settings of the considered method are established. Theoretical and experimental assessments on the advantages and accuracy of the variable-thickness approach are given based on comparison of the obtained solutions to the standard design for the plates with regular stiffening.
引用
收藏
页码:1787 / 1806
页数:20
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