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井下火箭发射燃气对消音层冲蚀损伤模型及特性
引用本文:李良,冯永保,马长林,夏文龙. 井下火箭发射燃气对消音层冲蚀损伤模型及特性[J]. 兵工学报, 2021, 42(4): 798-807. DOI: 10.3969/j.issn.1000-1093.2021.04.013
作者姓名:李良  冯永保  马长林  夏文龙
作者单位:(火箭军工程大学 导弹工程学院, 陕西 西安 710025)
基金项目:国家自然科学基金面上项目(51475462)
摘    要:井下火箭发射过程中消音层在发动机高温、高速燃气流作用下存在冲蚀损伤,会影响火箭发射安全,系统分析消音层燃气冲蚀损伤特性,对消音层的后期修复以及地下井结构优化具有重要意义.消音层冲蚀损伤是复杂的热-流体-固体多场耦合问题,以典型玻璃丝棉消音层为例,建立玻璃丝棉相变传热和烧蚀损伤数学模型;基于燃气流场数据提取与预处理、插值...

关 键 词:火箭发射  地下井  燃气流  玻璃丝棉  消音层  热-流体-固体耦合  烧蚀损伤

Model and Characteristics of Jet Flow Erosion Damage to Silencer Layer in Silo Launching Process of Rocket
LI Liang,FENG Yongbao,MA Changlin,XIA Wenlong. Model and Characteristics of Jet Flow Erosion Damage to Silencer Layer in Silo Launching Process of Rocket[J]. Acta Armamentarii, 2021, 42(4): 798-807. DOI: 10.3969/j.issn.1000-1093.2021.04.013
Authors:LI Liang  FENG Yongbao  MA Changlin  XIA Wenlong
Affiliation:(College of Missile Engineering, Rocket Force University of Engineering, Xi'an 710025, Shaanxi, China)
Abstract:The silencer layer is corrosively damaged by high temperature and high speed jet flow of rocket engine in the launching process. This affects the launching safety.The analysis of jet flow erosion damage is important to the late repair of silencer layer and the optimization of silo structure. The jet flow erosion damage to the silo silencer layer is a complicated thermal-hydro-mechanical coupling problem. The typical glass wool silencer layer is researched to build the phase change heat transfer and jet flow erosion damage mathematic models. A simulation platform of jet flow erosion damage is established by extracting and pretreating the jet flow field data, writing an interpolation program and developing Abaqus user subroutine. And a sub-model method is introduced to build a glass wool numerical simulation model. The ablation process of glass wool was simulated, the ablation damage was analyzed under the effects of silo diameter, initial height of jet flow and engine pressure build-up speed, and the simulation and ablation damage principle experiment for silo silencer layer were performed. The simulated results show that the glass wool silencer layer of the silo is generally damaged during jet flow ablation, which mainly occurs in the reverse flow and destabilizing stage. And the ablation damage is similar in the circumferential direction of the silo, but different in the axial direction. In addition, the damage is more serious closer to the bottom of silo, and the decreased diameter of silo or the increased pressure build-up speed of engine would aggravate ablation. But the increased initial height of jet flow will weaken ablation. The experimental results show that the glass wools are all damaged to a certain extent.
Keywords:rocketlaunching  silo  jetflow  glasswool  silencerlayer  thermal-hydro-mechanicalcoupling  ablationdamage  
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