期刊文献+

旋转爆轰的三维结构和侧向稀疏波的影响 被引量:10

Three-dimensional structure of rotating detonation and effect of lateral rarefaction waves
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摘要 基于带化学反应的三维Euler方程,采用氢气-空气的9组分19步基元反应简化模型,对圆环形燃烧室内的旋转爆轰进行了数值模拟,讨论了旋转爆轰波的三维结构及侧向稀疏波对旋转爆轰波阵面的影响。数值结果表明,爆轰波能够以旋转方式沿预混气层稳定传播。在侧向稀疏波作用下,爆轰波阵面发生变形。与理想的C-J爆轰相比,爆轰波强度和爆轰参数都有所下降。 Based on the multicomponent three-dimensional Euler equation, the phenomena of rotating detonation in the annular combustor were simulated numerically, and the three-dimensional structure of the rotating detonation wave and the effects of the lateral rarefaction waves on the detonation wave front were discussed. The numerical results show that the rotating detonation wave can propagate steadily in the layer of premixed gas, and the detonation wave front is distorted due to the lateral rarefaction nation waves. Compared with the ideal CJ detonation, the intensity and parameters of rotating detowave both decline somewhat.
出处 《爆炸与冲击》 EI CAS CSCD 北大核心 2010年第4期337-341,共5页 Explosion and Shock Waves
基金 国家自然科学基金项目(10872096) 北京理工大学爆炸科学与技术国家重点实验室开放基金项目(KFJJ09-13)~~
关键词 爆炸力学 三维结构 三维Euler方程 旋转爆轰 侧向稀疏波 mechanics of explosion three-dimensional structure three-dimensional Euler equation rotating detonation lateral rarefaction waves
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参考文献14

  • 1Roy G D, Frolov S M, Borisov A A, et al. Pulse detonation propulsion.. Challenges, current statues and future perspective[J]. Progress in Energy and Combustion Science, 2004,30:545-672.
  • 2Voitsekhovskii B V. Stationary detonation[J]. Doklady Akademii Nauk USSR, 1959,129(6):1254-1256.
  • 3Mikhailov V V, Topchian M E. To the studies of continuous detonation in an annular channel[J]. Combustion, Explosion, and Shock Wave, 1965,1(4) :12-14.
  • 4Bykovskii F A, Mitrofanov V V. Detonation combustion of a gas mixture in a cylindrical chamber[-J-. Combustion, Explosion, and Shock Wave, 1980,16(5) : 570-578.
  • 5Bykovskii F A, Mitrofanov V V. A continuous spin detonation Jn liquid fuel sprays[C]//Roy G D. Control of detonation processes. Moscow: Elex-KM, 2000:209-211.
  • 6Bykovskii F A, Zhdan S A, Vedernikov E F. Continuous spin detonations[J]. Journal of Propulsion and Power, 2006,22(6) :1204- 1216.
  • 7Lentsch A, Bec R, Serre L, et al. Overview of current French activities on PDRE and continuous detonation wave rocket engines[R]. AIAA 2005-3232, 2005.
  • 8Daniau E, Falempin F, Bykovskii F A, et al. Continuous detonation wave propulsion systems: First step toward operational engines[R]. ISABE 2005-1302, 2005.
  • 9Zhdan S A, Bykovskii F A, Vedernikov E F. Mathematical modeling of a rotating detonation wave in a hydrogenoxygen mixture[J]. Combustion, Explosion, and Shock Wave, 2007,43(4):449-459.
  • 10姜孝海,范宝春,董刚,陈志华,李鸿志.旋转爆轰流场的数值模拟[J].推进技术,2007,28(4):403-407. 被引量:29

二级参考文献18

  • 1董刚,于陆军,唐敖,范宝春.环形火焰引发爆震的数值研究[J].推进技术,2005,26(4):348-353. 被引量:6
  • 2Leveque R J.Wave propagation algorithms for multidimensional hyperbolic systems[J].Journal of Computarional Physics,1997,131:327-353.
  • 3Lu F K,Meyers J M,Wilson D R.Experimental study of a pulse detonation rocket with Shchelkin spiral[C]Jiang Z.Proceedings of the 24th International Symposium on Shock Waves Vol2.Beijing,China:Tsinghua University Press and Spring-Verlag Berlin Heidelberg,2005:825-830.
  • 4Roy G D,Frolov S M,Borisov A A,et al.Pulse detonation propulsion:Challenges,current starues and ruture perspective[J].Progress in Energy and Combustion Science,2004,30:545-672.
  • 5Tangirala V E,Dean A J,Chapin D M.Pulsed detonation engine processes:Axperiments and simulations[J].Combust Sci and Tech,2004,76:1 779-1 808.
  • 6Lieberman D H,Parkin K L,Shepherd J E.Detonation initiation by a hot turbulent jet for use in pulse detonation engines[R].AIAA 2002-3909.
  • 7Jackson S I,Grunthaner M P,Shepherd J E.Wave implosion as an initiation mechanism for pulse detonation engines[R].AIAA 2003-4820.
  • 8Lee J H S,Moen I O.The mechanism of transition from deflagration to detonation in vapor cloud explosions[J].Progress in Energy and Combustion Science,1980,6:359-389.
  • 9Nicholls J A,Wilkinson H R,Morrison R B.Intermediate detonation as a thrust-producing mechanism[J].Jet Propulsion,1957,27(5).
  • 10Danian E,Falempin F,Bykovskii F A,et al.Continuous detonation wave propulsion systems:first step toward operational engiues[R].ISABE 2005-1302.

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