| T300/BMP316层合板冲击后压缩强度试验 |
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| 引用本文： | 崔海坡,温卫东.T300/BMP316层合板冲击后压缩强度试验[J].航空动力学报,2008,23(11):2001-2006. |
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| 作者姓名： | 崔海坡 温卫东 |
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| 作者单位： | 上海理工大学医疗器械与食品学院;南京航空航天大学能源与动力学院; |
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| 摘 要： | 对两种不同铺层参数的T300/BMP316复合材料层合板进行了冲击后的剩余压缩强度试验研究.结果表明,虽然随着冲击能量的增加,层合板的剩余压缩强度逐渐降低,但二者之间不满足线性关系;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;层合板的剩余压缩强度与冲击损伤投影面积的大小没有直接关系.
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| 关 键 词： | 复合材料层合板 剩余压缩强度 冲击 试验 |
| 收稿时间： | 2007/10/22 0:00:00 |
| 修稿时间： | 2008/3/30 0:00:00 |
Post-impact compressive strength experiment of T300/BMP316 composite laminates |
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| CUI Hai-po and WEN Wei-dong.Post-impact compressive strength experiment of T300/BMP316 composite laminates[J].Journal of Aerospace Power,2008,23(11):2001-2006. |
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| Authors: | CUI Hai-po and WEN Wei-dong |
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| Institution: | CUI Hai-po1,WEN Wei-dong2(1.College of Medical Device , Food,University of Shanghai for Science , Technology,Shanghai 200093,China,2.College of Energy , Power Engineering,Nanjing University of Aeronautics , Astronautics,Nanjing 210016,China) |
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| Abstract: | Experiment study on impact damage and residual compressive strength had been done on T300/BMP316 composite laminates with different layer parameters.The results show that although the residual compressive strength gradually decreased with the increasing impact energy,there is no linear relationship between of them.The layer parameters has effect on the long-axis direction of impact damage figure,but hasn't influence on the impact damage area.The residual compressive strength has no direct relationship with ... |
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| Keywords: | composite laminates residual compressive strength impact experiment |
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