Nonlinear Stability of Filament-Wound Shells of Rocket Engine
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摘要:
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。
Abstract:
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.