本文简要介绍了玻璃钢在飞机头部雷达罩中的应用及其用纤维缠绕法成型的概况。
This paper introduces the method of fabrication of FRP nose radome by filament winding process.
碳纤维增强复合材料层剪强度测试结果表明，基体适用于纤维热熔法缠绕复合材料。
ILSS result of carbon fiber reinforced composite shows that the matrix is suitable for hot-melt carbon fiber winding composite material.
利用改进的剪切滞后法，研究了组成纤维缠绕压力容器中的环向层的横向开裂而在纵向层中引起的局部应变集中。
Local strain concentration in angle-ply lay caused by transverse crack of circular lay in composite pressure vessel was studied by means of advanced shear-lag method.
利用改进的剪切滞后法，研究了组成纤维缠绕压力容器中的环向层的横向开裂而在纵向层中引起的局部应变集中。
Local strain concentration in angle-ply lay caused by transverse crack of circular lay in composite pressure vessel was studied by means of advanced shear-lag method.
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