Modeling the forming process by successive local deforming for monolithic stiffened panels

被引:0
|
作者
Valeriy Sikulskiy
Stanislav Sikulskyi
Kateryna Maiorova
Yuri Dyachenko
机构
[1] National Aerospace University “Kharkiv Aviation Institute,Department of Aircraft Manufacturing
[2] Embry-Riddle Aeronautical University,Department of Aerospace Engineering
关键词
Stiffened monolithic panels; Forming; Local deforming; Panel deflection; Plastic deformation; Residual stress; Numerical modeling;
D O I
暂无
中图分类号
学科分类号
摘要
The study considers a method for forming stiffened monolithic panels by local deformation of the panel ribs. The local deformation is caused by bending moments along the rib towards each other. The goal of the study is to numerically model the forming process of the stiffened monolithic panel utilizing the designed local-impact tool and analyze its effects on the panel, obtaining which experimentally is challenging. The finite element method (FEM) modeling is performed in ANSYS and validated by the experimental forming of a panel made of an aluminum alloy analogous to Al 2024. Simulation results provide deformation, stress, and strain distributions along the panel in loaded and unloaded states for various study cases. Furthermore, the effects of finite panel length, width, and forming process parameters such as applied force couples and single versus successive deformation are numerically investigated and discussed. Performed modeling demonstrates the advantages of the forming with the designed tool in terms of low residual stresses and their distribution. Finally, the analysis suggests future modification of the tool, particularly the shape of its grips, to minimize local residual stress concentrations.
引用
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页码:1569 / 1578
页数:9
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