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固体火箭发动机金属壳体的破坏压强及其概率
引用本文:王铮.固体火箭发动机金属壳体的破坏压强及其概率[J].强度与环境,1994(1):44-50,F003.
作者姓名:王铮
作者单位:陕西动力机械研究所!西安,710000
摘    要:用弹塑性理论推导出以幂函数形式表示的高强钢制做的固体火箭发机壳体的塑性破坏压强及其概率计算公式,用断裂力学推导出壳体表面存在裂纹缺陷时的脆性破坏压强及其概率计算公式。

关 键 词:火箭发动机  金属壳体  屈服强度

Failure Pressure and Failure Probability of Metal Case for Solid Rocket Motor
Wang Zheng.Failure Pressure and Failure Probability of Metal Case for Solid Rocket Motor[J].Structure & Environment Engineering,1994(1):44-50,F003.
Authors:Wang Zheng
Institution:Shanxi Institute of Power Machinery
Abstract:Based on the theory of elasticity-plasticity, the computing formulas of plastic failure pressure and its probability of the solid rocket motor case which made by the high strength steel have been derived. The relationship between stress and straln of the high strength steel presents power function form.Based on the fracture mechanics, the formulas of brittle failure pressure and its probability of the motor case, whose surface has cracks, have been derived too.
Keywords:solid propellant rocket engines  metal shells  cylindrical shells  yield strength  fracture strength  structural reliability
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