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碳氢燃气超声速剪切流动燃烧数值模拟
引用本文:王慧,侯凌云.碳氢燃气超声速剪切流动燃烧数值模拟[J].航空动力学报,2007,22(4):559-564.
作者姓名:王慧  侯凌云
作者单位:清华大学,航天航空学院,北京,100084
摘    要:数值模拟碳氢富燃燃气与空气二维超声速剪切流动的湍流燃烧.NND对流项差分格式高精度捕捉激波,B-L和普朗特混合长度模型模拟湍流粘性系数,Arrhenius反应动力学公式计算化学反应速率,模拟非平衡态燃烧.计算的壁面压力值较好地符合了实验值.分析了剪切流驻焰稳定的波系结构,从预测的流动参数和组分浓度分布判断燃烧状况的好坏,从而为改善优化燃烧室结构提供工程参考.

关 键 词:航空、航天推进系统  超声速剪切流动  碳氢燃气燃烧  数值模拟  碳氢  燃气  超声速  剪切流动  燃烧数值模拟  shear  flow  supersonic  combustion  hydrocarbon  simulation  工程  波系结构  燃烧室  优化  改善  燃烧状况  判断  组分浓度分布  流动参数  预测
文章编号:1000-8055(2007)04-0559-06
收稿时间:2006/4/10 0:00:00
修稿时间:2006年4月10日

Numerical simulation of hydrocarbon gas combustion and supersonic shear flow
WANG Hui and HOU!Ling-yun.Numerical simulation of hydrocarbon gas combustion and supersonic shear flow[J].Journal of Aerospace Power,2007,22(4):559-564.
Authors:WANG Hui and HOU!Ling-yun
Institution:School of Aerospace, Tsinghua University, Beijing 100084, China;School of Aerospace, Tsinghua University, Beijing 100084, China
Abstract:A turbulent combustion of hydrocarbon fuel-rich gas with air two-dimensional supersonic shear flow was numerically simulated. NND difference scheme of convection item was used to capture shock wave with high precision, while turbulent viscid coefficient was calculated from B-L and Prandtl mixed length models. To simulate non-equilibrium combustion, Arrhenius reaction dynamic formula was used to confirm the chemical reaction rate. The simulated wall pressure results are in agreemant with the experimental data.The wave system suitable for flame stabilization was also analyzed.The combustion state was evaluated from the distribution of flow parameters and chemical components, providing a reference for improvement and optimization of combustion chamber.
Keywords:aerospace propulsion system  supersonic shear flow  hydrocarbon gas combustion  numerical simulation
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