论文:2014,Vol:32,Issue(1):23-28
引用本文:
白俊华, 胡春波, 李佳明. 固体发动机喷管喉衬流固耦合换热规律数值研究[J]. 西北工业大学
Bai Junhua, Hu Chunbo, Li Jiaming. The Numerical Research for Heat Transfer of Liquid-Solid Coupling on SRM Nozzle Throat[J]. Northwestern polytechnical university

固体发动机喷管喉衬流固耦合换热规律数值研究
白俊华, 胡春波, 李佳明
西北工业大学 燃烧 、 热结构与内流场重点实验室, 陕西 西安 710072
摘要:
通过考虑流场与壁面的湍流换热、固壁中的热传导以及包含吸收-发射性气体介质的喷管空腔中的热辐射交换等因素,建立了喷管喉衬流固耦合换热模型,通过与前人实验结果对照验证了模型的准确性;应用该模型分析了喷管粗糙度、燃气组分、燃烧室压强、推进剂燃温等因素对喷管喉衬热结构及换热规律的影响。仿真结果表明,喷管喉衬壁面温度和总热流密度在喷管喉部直段的前端达到最大;上述因素对喷管喉衬热交换的热流密度影响很大。
关键词:    数值模型    实验验证    数值仿真    喷管喉衬    壁面温度    热流密度   
The Numerical Research for Heat Transfer of Liquid-Solid Coupling on SRM Nozzle Throat
Bai Junhua, Hu Chunbo, Li Jiaming
Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:
The heat transfer liquid-solid coupling model was built by considering many factors,which are the turbulence heat exchange between flow and wall,the heat conduction of the wall and the thermal radiation exchange of the gas in the flow area. And the model was verified by the experiment results. The impacts of work conditions on throat heat structure were researched. The simulation results and their analysis indicate preliminarily that both the wall temperature and total heat flux of nozzle throat reach the highest values at the head of the straight segment,and such factors as roughness,gas composition,the pressure of combustion chamber and combustion temperature affect the total heat flux per unit time greatly.
Key words:    computer simulation    errors    experiments    heat conduction    heat flux    heat radiation    heat transfer    mathematical models    Navier-Stokes equations    numerical methods    pressure    rocket engines    rocket nozzles    schematic diagrams    solid propellants    surface roughness    temperature    temperature distribution    turbulent flow    nozzle throat    wall temperature   
收稿日期: 2013-05-02     修回日期:
DOI:
基金项目: 国家自然科学基金(50976095)资助
通讯作者:     Email:
作者简介: 白俊华(1983-),女,西北工业大学博士研究生,主要从事航空宇航推进理论与工程研究。
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