期刊文献+

脉冲爆震发动机数值模拟 被引量:1

Numerical simulation on pulse detonation engine
下载PDF
导出
摘要 为了获得脉冲爆震发动机(PDE)工作过程数值模拟技术,发展了DET2D程序,并以美国海军研究生院的气动阀式PDE为研究对象,进行了整机数值模拟。结果显示:所发展程序稳定、高效,可以用于多脉冲PDE流场的数值模拟及吸气式PDE数值模拟。通过计算,验证了PDE的工作原理和所发展程序的正确性。 To developed the numerical simulation technique of pulse detonation engine(PDE),the DET2D code was developed.By using the DET2D code,an whole engine computation has been rerformed for the NPS valveless PDE.The results show that the code is steady and efficient for multi-tube PDE and air breathing PDE.The results validate the principle of PDE operation and code.
出处 《推进技术》 EI CAS CSCD 北大核心 2010年第6期783-788,共6页 Journal of Propulsion Technology
关键词 脉冲爆震发动机 数值仿真 二维 Pulse detonation engine Numerical simulation 2D(Two-dimensional)
  • 相关文献

参考文献13

  • 1Paxson D E. A performance map for ideal air breathing pulse detonation engines[ R]. AIAA 2001-3465.
  • 2Ma F H. Thrust chamber dynamics and propulsive performance of airbreathing pulse detonation engines [ D ]. USA: Department of Mechanical and Nuclear Engineering , The Pennsylvania State University, 2003.
  • 3Fuhua Ma, Jeong-Yeol Choi. Internal flow dynamics and performance of valveless airbreathing pulse detonation engine[ R]. AIAA 2006-1024.
  • 4Fuhua Ma, Jeong-Yeol Choi, Vigor Yang. Internal flow dynamics in a valveless airbreathing pulse detonation combustor facility[ R]. A1AA 2007-1251.
  • 5Remeev N Kh, Vlasenko V V, Khakimov R A. Analysis of operation process and possible performance of the supersonic ramjet-type pulse detonation engine [ C ]. Moscow: Pulse and Continuous Detonation Propulsion, Torus Press, 2005:235 - 250.
  • 6Chang S C. The method of space-time conservation element and solution element : a new approach for solving the navier-stokes and euler equations [ J ]. Journal of Computational Physics, 1995 , 119.
  • 7HE Hao , Yu S-T J , ZHAN G Zeng-chan. Direct calculation of one-two-three-dimensional detonations by the CE/SE method[ R] . A1AA 2005-229.
  • 8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
  • 9Brown P N , Byrne G D , Hindmarsh A C. VODE: a variable coefficient ODE solver [J]. SIAM Journal on Scientific Computing, 1989 , 10 : 1038 - 1051.
  • 10Kee R J , Miller J A. Chemkin II: a fortran chemical ki- netics package for the analysis of gas-phase chemical kinetics[ R] . SAND 8928009B, 1989.

二级参考文献22

  • 1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
  • 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31

同被引文献15

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