中国舰船研究2024,Vol.19Issue(5) :158-165.DOI:10.19693/j.issn.1673-3185.03369

开圆孔波纹夹层板单向拉伸状态的应力极值优化求解

Stress extreme value optimization solution for infinitely corrugated core sandwich panel with circular opening under uniaxial tension

王小明 姜春萌
中国舰船研究2024,Vol.19Issue(5) :158-165.DOI:10.19693/j.issn.1673-3185.03369

开圆孔波纹夹层板单向拉伸状态的应力极值优化求解

Stress extreme value optimization solution for infinitely corrugated core sandwich panel with circular opening under uniaxial tension

王小明 1姜春萌2
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作者信息

  • 1. 中国舰船研究设计中心,湖北 武汉 430064
  • 2. 武汉船舶职业技术学院,湖北 武汉 430050
  • 折叠

摘要

[目的]旨在研究开圆孔无限波纹夹层板单向拉伸状态的应力分布,寻求最不利开孔位置.[方法]采用ANSYS软件子模型方法计算不同开孔位置的应力分布,并用ANSYS软件提供的零阶优化设计方法寻求最大应力集中系数时的开孔位置.[结果]开孔附近的应力分布与网格划分密切相关,最大应力总是出现在芯层板上.开圆孔无限波纹夹层板单向拉伸状态的应力集中系数普遍大于 3,最大可达 4.104.[结论]先整体模型再子模型的应力极值优化分析过程既可以节省计算时间,又可得到较高计算精度,提高优化效率.

Abstract

[Objective]In order to study the stress distribution of circular holed infinite corrugated core sandwich panels under uniaxial tension and seek the most unfavorable opening position,[Method]both submodel analysis method and subproblem optimization method were employed just for calculation stress dis-tribution of different holing positions and seeking the holing position where the hole edge stress concentration factor reached the maximum,respectively.[Result]The stress distribution near the opening is closely re-lated to the mesh division,and the maximum stress always occurs on the core layer board.The stress concen-tration factor of an infinitely corrugated sandwich panel with a circular opening under uniaxial tension is gen-erally greater than 3,with a maximum of 4.104.[Conclusion]Undergoing the stress extreme value optim-ization analysis process of the overall model before the submodel can save computation time,achieve high computational accuracy,and improve optimization efficiency.

关键词

开孔波纹夹层板/应力集中/孔边应力/极值优化求解

Key words

corrugated core sandwich panels with a hole/stress concentration/hole edge stress/extreme value optimization solution

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基金项目

国家部委基金资助项目()

出版年

2024
中国舰船研究
中国舰船研究设计中心

中国舰船研究

CSTPCDCSCD北大核心
影响因子:0.496
ISSN:1673-3185
参考文献量13
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