期刊文献+

等离子体点火对PDE一维两相爆轰影响的数值计算 被引量:9

Numerical Calculation of Influence of Plasma Ignition on PDE One-Dimensional Two-Phase Detonation
下载PDF
导出
摘要 建立了PDE管内利用等离子体射流点火过程的一维两相流体动力学数学模型,并用CE/SE方法对管内两相爆轰过程进行了数值模拟。分析讨论了等离子体射流点火不同射流时间及点火能量对于爆轰波形成的影响。结果表明:与常规火花点火相比,等离子体射流点火可以缩短DDT时间约35%,缩短DDT距离约30%;在能够形成爆轰的情况下,等离子体点火能量和点火时间的增加对DDT距离影响很小。计算结果对提高脉冲爆轰发动机的运行频率具有重要的参考价值。 A dynamics mathematical model of one-dimensional two-phase flow of transient plasma ignition (TPI) process was established in pulse detonation engine (PDE) tubes, and numerical simulation of two- phase detonation process in tubes was performed by use of CE/SE method. The influence of different jet ignition time and ignition energy of plasma jet ignition on detonation wave formation were analyzed and discussed. The results showed that compared with conventional spark ignition system, plasma jet ignition method is more effective. By means of plasma jet ignition method, DDT time can be decreased about 35%, and DDT distance can be decreased about 30%. Under the condition of detonation formation, the increases of plasma ignition time and ignition energy have little effect on DDT distance. All of these calculation results can provide important reference for improving the operating frequency of PDE.
作者 彭振 翁春生
出处 《火炮发射与控制学报》 北大核心 2009年第2期77-80,共4页 Journal of Gun Launch & Control
基金 国家自然科学基金资助(10672080)
关键词 流体力学 等离子体点火 脉冲爆轰发动机 两相爆轰 hydromechanics transient plasma ignition pulse detonation engine two-phase detonation
  • 相关文献

参考文献3

二级参考文献20

  • 1冯德成,翁春生,王震,白桥栋.点火管破孔的随机过程的一维两相流计算[J].爆炸与冲击,2004,24(6):481-486. 被引量:3
  • 2ChunshengWeng,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
  • 3陆欣,周彦煌.炮用发射装药点火管现状及未来发展趋势[J].弹道学报,1996,8(4):92-96. 被引量:3
  • 4谢多夫.力学中的相似方法与量纲理论(中译本)[M].北京:科学出版社,1982.235-267.
  • 5CHANGE S C. The method of space-time conservation dement and solution element - a new approach for solving the Navier-Stokes and Euler equations [ J]. Journal Computational Physics, 1995,119 : 295-324.
  • 6PARK S J,YU S T and LAI M C. Direct calculations of stable and unstable ZND detonations by the space-time conservation element and solution element method[R]. AIAA 98-3212.
  • 7CHANG S C, WANG X Y and CHOW C Y. New developments in the method of space-time conservation element and solution element-applications to two-dimensional time-marching problems[R]. NASA TM 106758,1994.
  • 8JAMES R .SCOTT and CHANG SIN-CHANG. The space-time solution element method-a new numerical approach for the Naver-Stokes equations[R]. AIAA-1995-0763.
  • 9ZHANGE Z C, JOHN S T,YU. etc. The CE/SE method for Naver-Stokes equations using unstructured meshes for flows at all speeds[R]. AIAA-2000-0393.
  • 10ZHANG ZENG-CHAN, JOHN S T. A modified space-time conservation element and solution element for Eider and Naver-Stokes equations[R]. AIAA 99-3277.

共引文献40

同被引文献76

引证文献9

二级引证文献51

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