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旋转爆轰胞格结构的实验和数值研究 被引量:12

Experimental and numerical investigation on cellular patterns of rotating detonations
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摘要 对爆轰波在环形圆管(预混气体为2H2/O2/Ar)内的传播分别进行了实验和数值研究。实验研究采用烟迹板记录了环形圆管内爆轰波的胞格结构。数值计算利用二阶附加半隐的Runge-Kutta法和五阶WE-NO格式分别离散欧拉方程的时间和空间导数项,采用基元反应简化模型描述化学反应过程,得到了旋转爆轰的流场及数值胞格结构。实验和数值模拟结果表明:爆轰波在圆环管中传播时,由于圆环的内壁发散、外壁收敛,圆环内侧爆轰强度小于外侧,胞格尺寸较大;内侧OH的分布区域大于外侧,浓度较低。旋转爆轰的这种性质,使爆轰波能以稳定的角速度绕轴旋转。 Gaseous detonation propagation of 2H2/O2/Ar mixture in an annular tube was experimentally and numerically investigated.Detonation cellular patterns were recorded by smoked foils.The second-order additive semi-implicit Runge-Kutta(ASIRK) method and the fifth-order weighted essentially non-oscillatory(WENO) scheme were used to discretize the time term and the spatial derivatives,respectively.A detailed chemical reaction mechanism model was applied to describe the processes of detonation chemical reactions.Numerical cellular patterns and detonation flow field were obtained.Experimental and numerical results show that while detonation propagates in the annular tube,due to the convergence of the outer wall and the divergence of the inner wall,the detonation intensity along the inner wall is lower than that along the outer wall,and the cell size is much larger.The distribution region of OH along the inner wall is also wider than that along the outer wall,and the concentration is smaller.Just because of the character of a rotating detonation,the detonation waves can rotate around an axis at a steady angular velocity.
出处 《爆炸与冲击》 EI CAS CSCD 北大核心 2011年第4期337-342,共6页 Explosion and Shock Waves
基金 国家自然科学基金项目(10872096) 国防弹道重点实验室基金项目~~
关键词 爆炸力学 旋转爆轰 二阶附加半隐的Runge-Kutta法 胞格结构 自持机理 mechanics of explosion rotating detonation second-order ASIRK method cellular pattern self-sustaining mechanism
作者简介 张旭东(1983-),男,博士研究生。
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参考文献16

  • 1Nicholls J A, Dabora E K, Gealler R A. Studies in connection with stabilized gaseous detonations waves[J]. Pro- ceedings of the Combustion Institute, 1959,11:766-772.
  • 2Voitsekhovskii B V. Stationary detonation[J]. Doklady Akademii Nauk Uz SSR, 1959,129 (6) : 1254.
  • 3Bykovskii F A, Vedernikov E F. Continuous detonation combustion of an annular gas-mixture layer[J]. Combus tion, Explosion, and Shock Waves, 1996,32:489 491.
  • 4Bykovskii F A, Vedernikov E F. Continuous detonation of a subsonic flow of a propellant[J]. Combustion, Explo- sion and Shock Wave, 2003,39(3):323-334.
  • 5Bykovskii F A, Zhdan S A, Vedernikov E F. Continuous spin detonation[J]. Journal of Propulsion and Power, 2006,22 : 1204-1216.
  • 6Daniau E, Falempin F, Zhdan S. Pulsed and rotating detonation propulsion systems: First step toward operational engines[R]. AIAA 2005-3233,2005.
  • 7Wolanski P, Kindracki J, Fujiwara T. An experimental study of small rotating detonation engine[C] // Roy G, Frolov S, Sinibaldi J. Pulsed and continuous detonations. Moscow: Torus press, 2006:332-338.
  • 8Zhdan S A, Bykovskii F A, Vedernikov E F. Mathematical modeling of a rotating detonation wave in a hydrogen- oxygen mixture[J]. Combustion, Explosion and Shock Waves, 2007,43(4):449-459.
  • 9Davidenko D M, GSkalp I, Kudryavtsev A N. Numerical study of continuous detonation wave rocket engine[R]. AIAA 2008 2680,2008.
  • 10Hishida M, Fujiwara T, Wolanski P. Fundamentals of rotating detonations[J]. Shock Waves, 2009,19..1 10.

二级参考文献9

  • 1Oran ES,Young TR,Boris JP,et al.Weak and strong ignition.I.Numerical simulation of shock tube experiments.J Combustion and Flame,1982,48:135~148
  • 2Takyama K,Honda M,Onodera O.Shock propagation along 90 degree bends.Rep Inst High Speed Mech,1977,35:83~111
  • 3Edwards DH,Fearnley P J,Nettleton MA.Shock's diffraction in channels with 90° bends.Journal of Fluid Mechanics,132:257~270
  • 4Thomas GO,Williams RL.Detonation interaction with wedges and bends.Shock Waves,2002,11:481~492
  • 5Zhong Xiaolin.Additive semi-implicit Runge-Kutta methods for computing high-speed nonequilibrium reactive flows.Journal of Computational Physics,1996,128:19~31
  • 6Shu Chiwang.Essentially non-oscillatory and weighted essentially non-oscillatory schemes for hyperbolic conservation laws.NASA/CR-97-206253,1997
  • 7Strehlow R.The nature of transverse waves in detonations.Astronautica Acta,1969,14:539~548
  • 8夏昌敬,周凯元,沈兆武,董永香,年伟民,王汉良.可燃气体非稳定爆轰波通过90°圆弯管传播特性的实验研究[J].实验力学,2002,17(4):438-443. 被引量:8
  • 9王昌建,徐胜利,郭长铭.气相爆轰波在半圆形弯管中传播现象的实验研究[J].爆炸与冲击,2003,23(5):448-453. 被引量:15

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