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 ％ 。
In order for the solution of the laminated plates and shells to ensure interlaminar continuity of the physical variables, the transfer matrix technique was used.
针对层合板壳问题，为了保证各层之间物理参量的连续性，进一步应用了状态转移矩阵技术。
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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