wound rocket
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In this paper we employed the nonlinear finite element method to calculate the stress and bursting pressure of filament wound rocket motor case.
本文采用大变形有限元方法进行纤维缠绕固体火箭发动机壳体的应力及爆破分析。
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In this paper we employed the nonlinear finite element method to calculate the stress and bursting pressure of filament wound rocket motor case.
摘 要 本文采用大变形有限元方法进行纤维缠绕固体火箭发动机壳体的应力及爆破分析。
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Following conclusions are concerning the strength of filament wound solid rocket motor case:(1) The inter-delamination is important for the strength of the case, and there are many factors, such as, the matrix, the interface, the fiber volume fraction, the fiber arrange pattern, to influence on the delamination.
最终结合宏观、细观两方面的研究和分析，并联系到纤维缠绕固体火箭发动机壳体的强度，可以得到如下结论：（1）壳体的内部脱层是导致壳体强度下降的重要原因，而影响壳体内部脱层的因素除了基体材料外还有界面，纤维的排列阵列、体积分数，壳体的铺层次序等。