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。

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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。

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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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