In the range of incident velocities near to the perforation limit velocity (V50), this mechanism depends on thickness and interlaminar shear strength of composite plate.
在接近穿孔极限速度的入射速度(V50)范围内，这一机制依赖于复合材料板的厚度和中间层剪切强度。
It was concluded that the interlaminar tensile strength of the composite is dominated by the bonding strength of the interface between fiber and matrix, not by lay-up orientation.
结果表明：该复合材料层间拉伸强度较少受到铺层取向的影响，而由纤维与基体的界面结合强度所控制。
The results show that the treatment makes the interlaminar shear strength of the composite increased 17.5% and the linear ablation rate decreased 58.6%.
得出，该方法是提高复合材料层间剪切强度和抗烧蚀性能的有效方法，它可使层间剪切强度提高17．5 ％ ，线烧蚀率减小58．6 ％ 。
The results show that the treatment makes the interlaminar shear strength of the composite increased 17.5% and the linear ablation rate decreased 58.6%.
得出，该方法是提高复合材料层间剪切强度和抗烧蚀性能的有效方法，它可使层间剪切强度提高17．5 ％ ，线烧蚀率减小58．6 ％ 。
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