Research on impact damage of T300/BMP-316 composite laminates

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

Chinese

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Research on impact damage of T300/BMP-316 composite laminates

更新时间：2026-07-07

- Research on impact damage of T300/BMP-316 composite laminates
- Vol. 22, Issue 5, (2007)
- 作者机构：
  
  南京航空航天大学能源与动力学院,南京,210016
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2007
- 稿件说明：
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WEN Wei-dong, CUI Hai-po, XU Ying. Research on impact damage of T300/BMP-316 composite laminates[J]. 2007, 22(5).
DOI：

WEN Wei-dong, CUI Hai-po, XU Ying. Research on impact damage of T300/BMP-316 composite laminates[J]. 2007, 22(5). DOI：

摘要

采用自由落体冲击设备

对两种不同尺寸不同铺层顺序的T300/BMP-316复合材料层合板进行了详细的低速冲击损伤试验研究

同时应用作者以前发展的复合材料层合板逐渐累积损伤分析方法对层板的冲击过程进行了模拟.结果表明

几何尺寸对层合板的冲击损伤投影面积有较大的影响

而铺层顺序对冲击损伤投影面积影响不大

但对层合板的冲击损伤形状会有一定的影响.

Abstract

The experimental research of low speed impact damage has been carried out on composite laminates with different geometries and layer direction angle

and the impact process was simulated by the progressive damage method.The geometries of composite laminates have much effect on the impact damage projected area.The layer direction angle of composite laminates has little effect on the impact damage projected area

but it has influence on the impact damage figure.

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Related Author

CUI Hai-po

WEN Wei-dong

XU Ying

ZHANG Guo-dong

YU Hui-chen

HE Yu-huai

SU Bin

SHI Duo-qi

Related Institution

Institute of Medical Device, University of Shanghai for Science and Technology

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

Beijing Institute of Aeronautical Materials, China Aviation Industry Corporation I

School of Jet Propulsion, Beijing University of Aeronautics and Astronautics

Department of Engineering Mechamics,Northwestern Polytechnical University

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