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粒子侵蚀下三元乙丙绝热材料炭化层破坏特性实验研究
引用本文:徐义华,胡春波,李江.粒子侵蚀下三元乙丙绝热材料炭化层破坏特性实验研究[J].工程力学,2011(5):251-256.
作者姓名:徐义华  胡春波  李江
作者单位:西北工业大学燃烧流动及热结构重点实验室;南昌航空大学飞行器工程学院;
基金项目:国家自然科学基金项目(50976095); 国家“973”基金项目(61371)
摘    要:应用模拟固体火箭发动机烧蚀环境的炭化层制样装置制备三元乙丙绝热材料炭化层,分析了三元乙丙绝热材料炭化层结构特点,并设计了一套粒子侵蚀装置,对侵蚀角度为30°、60°和90°工况进行了三元乙丙绝热材料炭化层的粒子侵蚀破坏试验,应用高速摄影系统记录粒子侵蚀炭化层过程,经过分析计算得出了炭化层的剪切极限强度和抗压极限强度,为...

关 键 词:航天推进系统  固体火箭发动机  粒子侵蚀  EPDM  炭化层  破坏特性

EXPERIMENTAL STUDY ON THE BREAKAGE CHARACTERISTIC OF CHARRING LAYER OF EPDM HEAT-INSULATING MATERIAL ERODED BY PARTICLE FLOW
XU Yi-hua,HU Chun-bo,LI Jiang.EXPERIMENTAL STUDY ON THE BREAKAGE CHARACTERISTIC OF CHARRING LAYER OF EPDM HEAT-INSULATING MATERIAL ERODED BY PARTICLE FLOW[J].Engineering Mechanics,2011(5):251-256.
Authors:XU Yi-hua  HU Chun-bo  LI Jiang
Affiliation:XU Yi-hua1,2,HU Chun-bo1,LI Jiang1(1.Key Laboratory of Combustion,Flow and Thermal-Structure,Northwestern Polytechnical University,Xi'an 710072,China,2.School of Aircraft Engineering,Nanchang Hangkong University,Nanchang 330063,China)
Abstract:The device which can simulate the thermal ablation in a solid rocket motor was used to make the sample of charring layer of Ethylene-Propylene-Diene Monomer(EPDM) heat-insulating material.The structure characteristics of charring layer were analyzed.A suit of device used for researching particle eroding charring layer of heat-insulating material was designed.It is carried out three tests of particle eroding EPDM charring layer with the erosion angles of 30°,60° and 90°,respectively.The process of erosion is recorded by high-speed camera.The velocity of eroding particle is gained by analyzing the image.The force particle acting on the charring layer is computed by the law of momentum.The limiting shearing and crushing stress is derived by comparing the testing data,which can be applied to the model ablation of EPAM under considering the eroding effect of gas and particle.
Keywords:propulsion system of aerospace  solid rocket motor  particle eroding  EPDM  charring layer  breakage characteristic  
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