复合材料板冲击损伤及剩余拉伸强度试验

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

1.
Institute of Medical Device, University of Shanghai for Science and Technology, Shanghai 200093, China
2.
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

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.
- 航空、航天推进系统 /
- 冲击 /
- 剩余拉伸强度 /
- 复合材料层合板 /
- 试验
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.
- aerospace propulsion system /
- impact /
- residual tensile strength /
- composite laminates /
- experiment

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