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脉冲爆震发动机倒旋流气动阀数值与实验研究
引用本文:宫继双,范育新,王家骅,占欢,张靖周.脉冲爆震发动机倒旋流气动阀数值与实验研究[J].航空动力学报,2011,26(8):1719-1727.
作者姓名:宫继双  范育新  王家骅  占欢  张靖周
作者单位:南京航空航天大学能源与动力学院,南京,210016
摘    要:为了减小脉冲爆震发动机爆震燃烧时气动阀的倒流量,提出一种倒旋流气动阀,给出了不同倒流旋流数下模型气动阀的流动分析.结果表明:对于几何尺寸给定的气动阀,存在一个最佳的旋流数,此时气动阀的单向阀性能最好,气动阀的最佳旋流数约为1.0.此外,设计了旋流数为1.364的气动阀,进行了实验,冷态实验结果验证了数值方法的可靠性;热态实验表明采用该气动阀可以在直径114 mm的爆震管获得频率为40 Hz稳定的爆震波.

关 键 词:脉冲爆震发动机  气动阀  倒旋流气动阀  旋流数  爆震频率
收稿时间:5/5/2010 12:00:00 AM
修稿时间:2010/8/27 0:00:00

Numerical and experimental study on inversing-rotating aero-valves of PDE
GONG Ji-shuang,FAN Yu-xin,WANG Jia-hu,ZHAN Huan and ZHANG Jing-zhou.Numerical and experimental study on inversing-rotating aero-valves of PDE[J].Journal of Aerospace Power,2011,26(8):1719-1727.
Authors:GONG Ji-shuang  FAN Yu-xin  WANG Jia-hu  ZHAN Huan and ZHANG Jing-zhou
Institution:GONG Ji-shuang,FAN Yu-xin,WANG Jia-hua,ZHAN Huan,ZHANG Jing-zhou(1.College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)
Abstract:As a new concept aero-valve used in pulse detonation engine(PDE),inversing-rotating aero-valve was mentioned to improve one-way performance of the valve in this paper.A useful inclusion was obtained after a series of numerical investigation,that is,the swirl number is the key parameter affected the valve's performance.The optimum value of swirl number is approximately one.In addition,an aero-valve which swirl number equals to 1.364 was made to experiment.The experimental results without ignition demonstrate...
Keywords:pulse detonation engine  aero-valve  inversing-rotating aero-valve  swirl number  detonation frequency  
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