航空兵器Issue(1)：40-43,4.
星型药柱固化降温瞬态热力耦合分析
The rmo-Mechanical Coupling Analysis of Star Grain in the Course of Cooling Process After Curing
肖志平 1张泽远 1邢国强1
作者信息
- 1. 中国空空导弹研究院，河南洛阳 471009
- 折叠
摘要
Abstract
The research on thermal stress produced in the course of cooling process after curing of SRM grain has important significance , owing to it has important influence on structural integrity of propel-lant.Considering effect of convective heat transfer , the thermo-mechanical coupling process of star grain during cooling course is simulated with the finite element software .The transient temperature distribution affected by time of cooling process is analyzed and thermal stress and strain for danger area is presented . In addition, the time needed in the cooling process after curing is acquired and the two results with differ-ent thermal boundary are compared and discussed as well .All the work is an available reference for struc-tural integrity analysis of propellant grains with thermal load applied .关键词
推进剂/固化降温/热力耦合/对流换热/数值仿真Key words
propellant grain/cooling process after curing/thermo-mechanical coupling/convective heat transfer/numerical simulation分类
航空航天引用本文复制引用
肖志平,张泽远,邢国强..星型药柱固化降温瞬态热力耦合分析[J].航空兵器,2014,(1):40-43,4.
