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稳定器流动、燃烧实验及冷态大涡模拟研究
引用本文:王方,许春晓,王家骅,范育新,韩启祥.稳定器流动、燃烧实验及冷态大涡模拟研究[J].航空动力学报,2006,21(3):502-506.
作者姓名:王方  许春晓  王家骅  范育新  韩启祥
作者单位:1.清华大学 航天航空学院, 北京 100084
摘    要:蒸发式V型稳定器是一种适用于加力式涡扇发动机加力燃烧室的外涵稳定器,本文在冷态实验中测量其流阻,同时在热态实验中测量其工作范围,并用大涡模拟对其冷态流场进行了三维全尺寸非稳态的数值模拟。分析表明,多处的回流区的组织有利于增加稳定器的稳定工作范围。 

关 键 词:航空、航天推进系统    蒸发式V型稳定器    大涡模拟    加力燃烧室
文章编号:1000-8055(2006)03-0502-06
收稿时间:2005/6/21 0:00:00
修稿时间:2005年6月21日

Experimental Studies of Flow and Combustion with a Flame-Holder and LES of the Flow
WANG Fang,XU Chun-xiao,WANG Jia-hu,FAN Yu-xin and HAN Qi-xiang.Experimental Studies of Flow and Combustion with a Flame-Holder and LES of the Flow[J].Journal of Aerospace Power,2006,21(3):502-506.
Authors:WANG Fang  XU Chun-xiao  WANG Jia-hu  FAN Yu-xin and HAN Qi-xiang
Institution:1.School of Aerospace, Tsinghua University, Beijing 100084, China2.College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:Flow and combustion in a combustor using a V-gutter flame-holder with pre-vaporization for afterburners are studied by experiments and the cold flow is also studied by large-eddy simulation.The results indicate that this kind of flame holder can create multiple recirculation zones which lead to increasing the range of flame stabilization.
Keywords:aerospace propulsion system  V-gutter flame-holder with pre-vaporization  large-eddy simulation  afterburner
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