期刊文献+

基于WENO格式的爆震波传播过程一维数值模拟 被引量:1

One Dimensional Numerical Study of Detonation Wave with WENO Scheme
下载PDF
导出
摘要 用时间算子分裂法来分离普通流体流动和化学反应方程,采用有限体积加权基本无振荡格式构建了带有复杂状态方程的欧拉方程组;提出一种新的熵修正方法EF4,并结合Roe平均格式来解决激波的不稳定问题和间断问题。通过对带有详细化学反应的爆震波传播过程进行了一维数值模拟,获得的爆震波稳定压力以及爆震波传播速度都和理论结果一致,结果表明,WENO有限体积格式可以很好地模拟爆震波传播过程。 Using time operator splitting technique and weighted essentially non - oscillatory ( VCENO ) schemes to simulate detonation with detailed chemical reaction, a time operator splitting technique is employed to decouple hydra - dynamic transport and chemical reaction, and finite volume VCENO scheme is constructed for the homogeneous Euler equations with complex equation of state. And a new entropy correction method EF4 is proposed to solve the problem of the shock instability in combination with Rose scheme. The obtained front pressure and velocity of detonation waves are in good agreement with the theoretic results, the results show that the VCENO finite volume scheme can be used to simulate the transmitting process of the detonation wave perfectly.
出处 《空军工程大学学报(自然科学版)》 CSCD 北大核心 2008年第2期18-21,共4页 Journal of Air Force Engineering University(Natural Science Edition)
基金 国家自然科学基金资助项目(50276070)
关键词 时间算子分裂法 加权基本无振荡格式 有限体积 爆震波 激波 time operator splitting WENO scheme finite volume detonation wave shock wave
  • 相关文献

参考文献10

  • 1Strehlow R A. Gas Phase Detonations : Recent Developments [ J]. Combustion Flame, 1969,12 (2) : 539 - 548.
  • 2王丁喜,严传俊.爆震燃烧波在管内传播过程的二维数值模拟[J].机械科学与技术,2006,25(4):461-464. 被引量:5
  • 3刘云峰,王健平.有限谱ENO格式在爆轰波数值模拟中的应用[J].爆炸与冲击,2003,23(4):343-348. 被引量:6
  • 4Kim Hyungwon. Numerical Simulation of Transient Combustion Process in Pulse Detonation Engine[ R ]. AIAA ,2000.
  • 5Schwer D A. Numerical Study of Unsteadiness in Non - reactiong and Reacting Mixing Layer[ D]. The Pennsylvania State University ,2000.
  • 6Jiang G S, Shu C W. Efficient Implementation of Weighted ENO Schemes [ J]. Comput Phys, 1996,126:202 -228.
  • 7Oran E S, Weber J W, Stefaniw E I, et al. A Numerical Study of a 2D H2 - 02 - Ar Detonation Using a Detailed Chemical Reaction Model[ J ]. Combustion and Flame, 1998,113 : 147 - 163.
  • 8Deiterding R. Numerical Structure Analysis of Regular Hydrogen - Oxygen Detonations : The Fall 2003 Meeting of the Western States Section [ C ]. Los Angles : The Combustion Institute,2003.
  • 9陈永刚,何立明,康强,李明奎.基于特征线的脉冲爆震发动机性能估算与结构参数设计[J].空军工程大学学报(自然科学版),2005,6(3):1-3. 被引量:3
  • 10胡杰,黄长强,和黎伟.脉冲火箭弹模型仿真[J].空军工程大学学报(自然科学版),2007,8(2):26-28. 被引量:3

二级参考文献31

  • 1吴媛媛,吴进华,唐静.基于Matlab的导弹飞行动力学仿真模型库设计[J].海军航空工程学院学报,2005,20(2):257-260. 被引量:5
  • 2史金光,王中原,刘巍,李汝亭.简易控制修正力技术研究[J].弹道学报,2006,18(1):14-17. 被引量:8
  • 3Kuo K K. Principles of combustion[M]. New York:John Wiley & Sons, 1986:261--266.
  • 4Taki S, Fujiwara T. Numerical analysis of two-dimensional nonsteady detonation[J]. American Institute of Aeronautics and Astronautics Journal, 1978,16(1) : 73 -- 77.
  • 5WANG Jian-ping. Finite spectral method based on non-periodic Fourier transform[J]. Computers & Fluids, 1998,27(5/6): 639--644.
  • 6WANG Jian-ping. Key to problems in spectral methods[A]. Hafez M, Oshima K. Computational Fluid Dynamics Review 1998[C]. Singapore: World Scientific, 1998: 369--378.
  • 7Sharpe G J. Transverse waves in numerical simulations of cellular detonations [J]. Journal of Fluid Mechanics,2001,447:31--51.
  • 8Strehlow R A, Adamczyk A A, Stiles R J. Transient studies of detonation waves[J]. Astronautica Acta, 1972,17(4/5):509--527.
  • 9WANG Jian-ping. Finite spectral method for compressible and incompressible flows[J]. Computational Fluid Dynamics Journal, 2002,10(4): 569--574.
  • 10Eidelman S, Grossmann W, Gunners, N E, et al. Progress in pulsed detonation engine development[R]. American Institute of Aeronautics and Astronautics Paper 94-2721, 1994.

共引文献12

同被引文献13

引证文献1

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