主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
基于ABAQUS的加筋球壳参数化建模及屈曲分析
作者:
作者单位:

1.上海交通大学机械与动力工程学院;2.上海交通大学航空航天学院

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V223

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Parametric Modeling and Buckling Analysis of Stiffened Spherical Shell Based on ABAQUS
Author:
Affiliation:

1.Shanghai Jiao Tong University School of Mechanical Engineering;2.Shanghai Jiao Tong University School of Aeronautics and Astronautics

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    摘要:

    加筋球壳结构由于良好的承载能力和可设计性,其加筋设计及屈曲分析一直是经典且具有挑战性的问题。本文给出基于ABAQUS 的加筋球壳的参数化有限元建模方法,建立加筋球壳的参数化有限元模型;通过与文献数据进行比较对模型的准确性进行验证;以临界屈曲压力和临界屈曲压力与重量的比值为主要指标,研究球壳厚度,加强筋布局,加强筋截面尺寸等参数对铝合金加筋球壳屈曲的影响。结果表明:本文给出的方法提高了有限元建模效率;纬向筋对结构整体屈曲的的影响较为显著,而经向筋的影响则并不明显,增加球壳厚度与加强筋截面高度也能有效提高加筋球壳结构的屈曲性能。

    Abstract:

    Due to the good pressure capacity and designability, the stiffener design and buckling analysis of stiffened spherical shell have always been classic and challenging problems. In this paper, the parametric finite element modeling method of stiffened spherical shell based on ABAQUS is given, and the parametric finite element model of the stiffened spherical shell is established, which greatly improves the efficiency of the finite element modeling.. The accuracy of the model is verified by comparing with literature data. Using the critical buckling pressure Pc and the critical buckling pressure to weight ratio Pc/W as main indexes, the influence of shell thickness, stiffener layout, stiffener section size and other parameters on the buckling of aluminum alloy stiffened spherical shell is studied. The finite element analysis results show that circumferential stiffener has more significant influence on the overall buckling of the structure, while the influence of meridional stiffener is not obvious. Increasing the shell thickness and the section height of the reinforcement can also effectively improve the buckling performance of the stiffened spherical shell.

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引用本文

彭宇辰,陈秀华,吴亚东.基于ABAQUS的加筋球壳参数化建模及屈曲分析[J].航空工程进展,2022,13(5):123-130,170

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历史
  • 收稿日期:2021-11-03
  • 最后修改日期:2022-01-12
  • 录用日期:2022-02-11
  • 在线发布日期: 2022-07-25
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