期刊文献+

脉冲爆轰发动机进气压力对爆轰影响的实验研究 被引量:18

Experimental Study on Effect of Inlet Pressure on Detonation in Pulse Detonation Engine
在线阅读 下载PDF
导出
摘要 为了研究脉冲爆轰发动机进气压力对爆轰过程的影响,对以汽油空气混和物为燃料的脉冲爆轰发动机进行了实验研究.实验得到了工作频率为33Hz和40Hz的稳定爆轰波,其峰值压力分别为1.5~1.8MPa和1.3~1.8MPa.实验结果表明,空气进口压力对点火起爆过程及爆轰频率等具有大的影响,当进口空气压力降低,点火起爆过程变难,爆轰频率下降.实验结果对脉冲爆轰发动机机理研究及实验装置改进等具有一定的参考价值. In order to investigate the effect of inlet pressure on detonation in Pulse Detonation Engine (PDE), the experiments were done. It was filled with the mixture of gasoline and air in PDE. The steady detonation at the frequency of 33 Hz and 40 Hz was acquired, and their peak pressures are 1.5-1.8 MPa and 1.3-1.8 MPa respectively. The experiments indicate that the air inlet pressure have important effects on ignition process, detonation process, and frequency of detonation. When the inlet pressure is reduced, ignition process and detonation process get difficult, and frequency of work will drop. The results have important value on mechanism research and improvement of experiment device about PDE.
出处 《弹道学报》 CSCD 北大核心 2008年第3期1-4,共4页 Journal of Ballistics
基金 国家自然科学基金项目(10672080)
关键词 脉冲爆轰发动机 爆轰波 点火 进气压力 PDE detonation wave ignition inlet pressure
  • 相关文献

参考文献5

二级参考文献47

  • 1ChunshengWeng,JayP.Gore.A numerical study of two-and three-dimensional detonation dynamics of pulse detonation engine by the CE/SE method[J].Acta Mechanica Sinica,2005,21(1):32-39. 被引量:20
  • 2韩启祥.[D].南京:南京航空航天大学,2004,61~75.
  • 3Helman D. Detonation pulse engine[R]. AIAA 86-1683,1986.
  • 4Hinkey J. Rotary-Valved ,Multiple-Cycle,Pulse detonation engine experimental demonstration[R]. A-IAA 97-2746,1997.
  • 5Kentifield J A C. The noise producing characteristics of highly loaded valveless pulse combustor [R].ASME 86-WA/NCA-34 DEC, 1986, 103- 109.
  • 6Bertin J H. Aerodynamic valved [P]. U.S. Patent No. 2,670,011,54,1984.
  • 7Wislicenus G F. Flow control means for pulsejet combustion units[P]. US Patent No. 2,618,925,52,1982.
  • 8Srnirnov N N. Control of detonation onset in combustion gases [A]. High-Speed Deflagration and Detonation: Fundamentals and Control [C].Moscow, 2001.3-30.
  • 9Ashasov O V, Penyazkov O G. Some gasdynamic methods for control of detonation initiation and propagation[R]. AIAA 2001-3614,2001.
  • 10Levin V A. A new approach to organizing operation cycles in pulse detonation engines [A]. High-Speed Deflagration and Detonatioh: Fundamentals and Control[C]. Moscow, 2001. 223-238.

共引文献39

同被引文献204

引证文献18

二级引证文献53

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部