期刊文献+

CE/SE法模拟爆震波点火及传播过程 被引量:3

Numerical simulation of detonation ignition and propagation progress by CE/SE method
下载PDF
导出
摘要 运用时空守恒元和解元(CE/SE)法模拟一维爆震波的形成及传播过程,分析产生爆震波的不同机理和DDT(爆燃-爆震转捩)过程的影响因素.采取激波点火和热点点火两种点火方式,分别对应SDT(激波-爆震转捩)和DDT过程,热点点火初始场采用线性温度分布和阶梯性温度分布,整个管道均为常压.用隐式梯形方法实现刚性源项积分.结果表明,SDT和DDT对应于不同的爆震波机理,并且DDT受点火区不同参数的影响,为研究爆震波点火和DDT过程提供了理论依据. A space-time conservation element and solution element method (CE/SE) was used to simulate the formation and propagation process of one-dimensional detonation; also the detonation mechanism and influential factors to DDT (deflagration to detonation transition) were analyzed. Shock ignition method and hotspots ignition method, corresponding to SDT (shock to detonation transition) and DDT respectively, were employed. For the hotspot ignition, the initial pressure was 1 atm and temperature was linear or step-wise. Implicit trapezoidal technique was employed to handle stiff source term. Results show that the shock ignition and hotspot ignition are of different detonation mechanisms and DDT is affected by parameter variations in ignition zone. The results will offer reference to study of detonation ignition and DDT process.
出处 《航空动力学报》 EI CAS CSCD 北大核心 2008年第2期244-250,共7页 Journal of Aerospace Power
关键词 航空、 航天推进系统 时空守恒元和解元方法(CE/SE) 爆震波 点火 爆燃-爆震转捩(DDT) 激波-爆震转捩(SDT) aerospace propulsion system space-time conservation element and solution element method (CE/SE) detonation wave ignition deflagration to detonation transition (DDT) shock to detonation transition (SDT)
  • 相关文献

参考文献8

  • 1翁春生,Tay P Gore.CE/SE方法在非定常爆轰计算中的应用[J].空气动力学学报,2003,21(3):301-310. 被引量:16
  • 2陈永刚,何立明,刘建勋.时空守恒元和解元方法的爆震波一维数值模拟[J].推进技术,2005,26(3):256-259. 被引量:5
  • 3Chang S C. The method of space-time conservation element and solution: A new approach for solving the Navier-Stokes and Euler equations[J]. Journal Computational Physics, 1995,119:295-324.
  • 4HAO he, Yu S T J. Direct calculation of one-, two, there-dimensional detonations by the CESE method [R]. AIAA 2005-229,2005.
  • 5Kyoung-Su I, Yu S T J. Application of the CESE method to detonation with realistic finite-rate chemicemistry [R]. AIAA 2002-1020,2002.
  • 6WU Yuhui, YANG Vigor. Numerical simulation of detonation with detailed chemical kinetics using the space-time method[R]. AIAA 2000-0317,2000.
  • 7Bussing T, Pappas G. An introduction to pulse detonation engines[R]. AIAA 94-0263,1994.
  • 8Wintenberger E. Application of steady and unsteady detonation wave to propulsion[D]. California: California Institute of Techology Pasadena,2004.

二级参考文献18

  • 1严传俊,刘军,范玮,何立明,雷恒仁,王绍卿.脉冲爆震发动机工作原理与循环分析[J].推进技术,1996,17(3):56-63. 被引量:19
  • 2CHANGE 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.
  • 3PARK 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.
  • 4CHANG 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.
  • 5JAMES 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.
  • 6ZHANGE 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.
  • 7ZHANG ZENG-CHAN, JOHN S T. A modified space-time conservation element and solution element for Eider and Naver-Stokes equations[R]. AIAA 99-3277.
  • 8YU SHENC,--TAO, CHANG SIN-CHUNG. Treatments of stiff source terms in conservation laws by the method of space-time conservation element & solution element[R]. AIAA 97-0435.
  • 9ZHANG Z C,JOHN S T YU. A generalized space-time CE/SE method for the ELder equations on quadrilateral and hexagonal meshes[R]. AIAA-2001-2592.
  • 10COOPE M, JACKSON S, AUSTIN J E. Wintenberger and J. E. Shepherd. Direct experimental impulse measureamnts for detonations and deflagrations[R]. AIAA 2001-3812.

共引文献17

同被引文献49

引证文献3

二级引证文献7

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