Experimental research on impact damage and residual tensile strength of composite laminates

CUI Hai-po; WEN Wei-dong; XU Ying

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Experimental research on impact damage and residual tensile strength of composite laminates

更新时间：2026-07-07

- Experimental research on impact damage and residual tensile strength of composite laminates
- Vol. 22, Issue 10, (2007)
- 作者机构：
  
  1. 上海理工大学医疗器械学院,上海,200093
  2. 南京航空航天大学能源与动力学院, 南京 2l00l6
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2007
- 稿件说明：
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CUI Hai-po, WEN Wei-dong, XU Ying. Experimental research on impact damage and residual tensile strength of composite laminates[J]. 2007, 22(10).
DOI：

CUI Hai-po, WEN Wei-dong, XU Ying. Experimental research on impact damage and residual tensile strength of composite laminates[J]. 2007, 22(10). DOI：

摘要

T300/BMP316是一种很有应用前景的航空航天结构复合材料

对两种不同铺层参数的T300/BMP316复合材料层合板进行了冲击损伤及剩余拉伸强度试验.结果表明

不同铺层参数对层合板冲击损伤投影图形的长轴方向有一定的影响

但对冲击损伤投影面积大小几乎没有影响

层合板的剩余拉伸强度与冲击损伤投影面积的大小没有直接关系.

Abstract

T300/BMP316 is a promising composite on aeronautic and aerospace structures.The experimental research was performed on impact damage and residual tensile strength of T300/BMP316 composite laminates with different layer parameters.The results show that

layer parameters have effect on long-axis direction of impact damage figure

rather than the impact damage area.The residual tensile strength of laminates is not directly related to the impact damage area.

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Related Author

CUI Hai-po

WEN Wei-dong

WANG Dan-yong

CUI Hai-po

XU Ying

GUO Wen

JI Hong-hu

Related Institution

College of Medical Device and Food, University of Shanghai for Science and Technology

College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics

China North Indnstries Group Corporation Institute 53

College of Medical Devices, University of Shanghai for Science and Technology

College of Energy and Powr Engineering,Nanjing University of Aeronautics and Astronautics

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