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碳/酚醛材料的粒子侵蚀
引用本文:高立新,蔡峨.碳/酚醛材料的粒子侵蚀[J].推进技术,1993,14(5):31-38.
作者姓名:高立新  蔡峨
作者单位:北京航空航天大学 (高立新),北京航空航天大学(蔡峨)
摘    要:引用均质材料的冲蚀疲劳理论,研究了碳/酚醛材料应用在固体火箭发动机喉衬情况下的侵蚀特性;分别对无碳化层和有碳化层两种状态进行了分析和计算。综合热化学烧蚀计算与实验对比,得到粒子冲蚀的定性定量结果。

关 键 词:固体推进剂  火箭发动机  喷管  衬套

PARTICLE IMPINGEMENT OF CARBON/ PHENOLIC MATERIALS
Gao Lixin and Cai E.PARTICLE IMPINGEMENT OF CARBON/ PHENOLIC MATERIALS[J].Journal of Propulsion Technology,1993,14(5):31-38.
Authors:Gao Lixin and Cai E
Institution:Beijing University of Aeronautics and Astronautics
Abstract:In this paper theorems on homogeneous materials subjected to impingements and fatigue was quoted. Erosive behavior of C/phenolic materials applied to solid rocket nozzle throats was investigated. Analysis and calculation on a single substrate and substrate covered by a changing char layer was conducted respectively. Sum up the thermo-chtr cal erosion calculation and contrast with the test results, the qualitative and quantitative results of particle impingements were gained.
Keywords:Solid propellant rocket engine  Nozzle liner  Fiber reinforced composite  Impingement corrosion  
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