Stress analysis of solid propellant motor when temperature varys in storage is presented in this paper. A viscoelastic finite element model based on integral creep constitutive relation is obtained and the method is applid to the thermal stress analysis of viscoelastic beam, cylinder and solid propellant motor.
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冯志刚,周建平.固体火箭发动机长期贮存热载荷的有限元分析方法[J].国防科技大学学报,1994,16(2):67-71. Feng Zhigang, Zhou Jianping. The Thermal Stress of the Solid Rocket Motor Grain in Storage[J]. Journal of National University of Defense Technology,1994,16(2):67-71.