固体火箭发动机药柱三维粘弹性摄动随机有限元分析

3D VISCOELASTIC PERTURBATION STOCHASTIC FINITE ELEMENT ANALYSIS OF SOLID ROCKET MOTOR GRAIN

  • 摘要: 发展了一种三维粘弹性摄动随机有限元法(VPSFEM),并对固体火箭发动机药柱进行了随机分析。以不可压和近似不可压粘弹性有限元方法为基础,采用一阶随机摄动技术处理结构分析参数的随机性,推导了三维粘弹性摄动随机有限元方法的递归方程组,并给出了结构响应统计特征的求解方法。推导过程中同时考虑了材料力学性能和载荷环境参数的随机性。算例分析中对典型载荷作用下的固体火箭发动机药柱结构进行了三维随机分析,结果表明三维粘弹性摄动随机有限元方法效率高,且精度能够满足工程需要。

     

    Abstract: A kind of three-dimension viscoelastic perturbation stochastic finite element method (VPSFEM) was developed, and then the VPSFEM method was applied in the stochastic analysis of solid rocket motor grains. Based on the incompressible and nearly incompressible viscoelastic finite element methods, uncertainties associated with structural parameters were dealt with using the first-order stochastic perturbation technique, and recursive formulations of viscoelastic perturbation stochastic finite element method were derived. The method for evaluating statistical characters of structural responses was also presented. The randomness of solid propellant mechanics properties and loads was taken into account in the derivation. The 3D stochastic analysis of solid rocket motor grain under typical loads was performed. The simulated results show that the 3D viscoelastic perturbation stochastic finite element method is efficient, and its accuracy can meet the requirement of engineering projects.

     

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