结合算例说明了该方法在固体火箭发动机结构完整性分析中的适用性。
Calculating examples are given to illustrate the application of the method on structure integral analysis of solid rocker motor.
根据航空发动机结构完整性大纲，对于断裂关键件必须进行损伤容限设计分析。
According to aeroengine structure integrity program, fracture critical components must be analysed with damage tolerance concept.
该文的结果对固体火箭发动机装药结构完整性分析计算有重要的实用价值。
The results of this paper are of practical significance to grain structural integrity analysis and computation of solid rocket engines.
通过计算温度场和应力场，分析了喷管在发动机工作过程中的结构完整性。
Structure integrality of nozzle during the working process of motor was analyzed by calculating temperature field and stress field.
固体火箭发动机药柱结构完整性分析及贮存寿命预估是设计、生产和使用部门非常关注的关键问题。
Structural integrity analysis and storage life prediction of grain is a critical problem for the designers, manufacturers and users of Solid Rocket Motor (SRM).
因此，进行含随机参数固体火箭发动机药柱结构完整性分析及贮存寿命预估研究具有重要的理论意义和应用价值。
Therefore, it is of important value both on theory and application to research structural integrity analysis and storage life prediction of SRM grain with random parameters.
因此，进行含随机参数固体火箭发动机药柱结构完整性分析及贮存寿命预估研究具有重要的理论意义和应用价值。
Therefore, it is of important value both on theory and application to research structural integrity analysis and storage life prediction of SRM grain with random parameters.
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