纤维缠绕火箭发动机外壳的非线性稳定

Nonlinear Stability of Filament-Wound Shells of Rocket Engine

应用复合材料的理论，对纤维缠绕圆柱壳的稳定性进行了分析，提出了壳体在轴向压缩下的临界载荷的算法．

Based on the theory of composite, the analysis of stability of filamentwound circular cylindrical shells is performed. A algorithm for calculating the critical load under axial pressure is presented.