| 含损伤复合材料层合板剩余压缩强度研究进展 |
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| 引用本文： | 郑锡涛,李泽江,李光亮.含损伤复合材料层合板剩余压缩强度研究进展[J].宇航材料工艺,2011,41(3). |
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| 作者姓名： | 郑锡涛 李泽江 李光亮 |
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| 作者单位： | 西北工业大学航空学院,西安,710072 |
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| 摘 要： | 综述了含损伤复合材料层合板剩余压缩强度的研究进展,重点介绍受低速冲击后复合材料层合板的剩余压缩强度问题,主要包括:(1)层合板压缩失效的损伤特征及损伤状态表征;(2)层合板压缩试验研究;(3)损伤模型分析及失效分析;(4)研究展望.
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| 关 键 词： | 复合材料层合板 剩余压缩强度 损伤 进展 |
Advance of Study on Residual Compressive Strength of Damaged Composite Laminates |
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| Zheng Xitao,Li Zejiang,Li Guangliang.Advance of Study on Residual Compressive Strength of Damaged Composite Laminates[J].Aerospace Materials & Technology,2011,41(3). |
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| Authors: | Zheng Xitao Li Zejiang Li Guangliang |
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| Institution: | Zheng Xitao Li Zejiang Li Guangliang(School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072) |
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| Abstract: | Advances in damage analysis for composite laminates are summarized.Emphasis is placed on the residual compressive strength of the damaged composite laminates after low velocity impact in composite engineering structures.The contents of the article are as follows:(1)damage characteristic of laminates compressive failure.(2)laminates compressive experimentation.(3)damage model analysis and failure analysis.(4)perspective for developing new analysis methods. |
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| Keywords: | Composite laminates Residual compressive strength Damage Advance |
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