CN117275633B - 一种航空复合材料结构破坏过程分析方法及计算机设备 - Google Patents
一种航空复合材料结构破坏过程分析方法及计算机设备 Download PDFInfo
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CN117494534B (zh) * | 2024-01-03 | 2024-03-22 | 南京航空航天大学 | 一种基于点云与有限元分析的飞机蒙皮修配方法 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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CN107688686A (zh) * | 2017-07-07 | 2018-02-13 | 中国航空工业集团公司西安飞机设计研究所 | 一种基于弹脆性损伤模式的层压板结构破坏模拟方法 |
CN111709174A (zh) * | 2020-06-18 | 2020-09-25 | 江南大学 | 一种基于失效面理论的复合材料层合板强度分析方法 |
WO2021248850A1 (zh) * | 2020-06-11 | 2021-12-16 | 大连理工大学 | 强度准则驱动的近场动力学模型预测结构破坏的方法 |
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Publication number | Priority date | Publication date | Assignee | Title |
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CN107688686A (zh) * | 2017-07-07 | 2018-02-13 | 中国航空工业集团公司西安飞机设计研究所 | 一种基于弹脆性损伤模式的层压板结构破坏模拟方法 |
WO2021248850A1 (zh) * | 2020-06-11 | 2021-12-16 | 大连理工大学 | 强度准则驱动的近场动力学模型预测结构破坏的方法 |
CN111709174A (zh) * | 2020-06-18 | 2020-09-25 | 江南大学 | 一种基于失效面理论的复合材料层合板强度分析方法 |
Non-Patent Citations (2)
Title |
---|
Computational methods for predicting impact damage in composite structures;A.F Johnson;ScienceDirect;全文 * |
基于弹塑性损伤本构模型的复合材料层合板破坏荷载预测;陈静芬;;复合材料学报(第04期);全文 * |
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Inventor after: Dong Leiting Inventor after: Li Mingjing Inventor after: Dai Xueyan Inventor after: Shen Baoying Inventor after: Wang Kailei Inventor after: Wang Song Inventor before: Li Mingjing Inventor before: Dai Xueyan Inventor before: Shen Baoying Inventor before: Wang Kailei Inventor before: Wang Song Inventor before: Dong Leiting |