期刊文献+
任意字段
题名或关键词
题名
关键词
文摘
作者
第一作者
机构
刊名
分类号
参考文献
作者简介
基金资助
栏目信息

固体火箭发动机大尺度多相内流场的大涡模拟

Large Eddy Simulation of Large Scale Multiphase Flow for Solid Rocket Motor
下载PDF
导出
摘要 使用大涡模拟方法对含有铝液滴和氧化物烟雾的固体火箭发动机复杂多相湍流流场进行了数值模拟研究,在大涡模拟中使用Smagorinsky涡黏模型计算亚格子尺度应力张量。拉格朗日方法被用来实时跟踪铝液滴在流场中的位置和速度,同时采用平衡欧拉近似方法计算烟雾的速度场,并利用这个速度场求解描述烟雾浓度的对流扩散方程。最后,使用该计算模型对某型SRM进行了数值模拟,结果给出了正确的流场结构,显示出计算模型的正确性。 Large eddy simulation method was employed to carry out numerical research on complex multiphase turbulent flow containing Al droplets and resulting oxide smoke inside solid rocket motor （SRM）. Smagorinsky eddy viscosity formulation was used to calculate sub-grid scale stress tensor. The velocity and position of Al droplets was tracked with Lagrangian method in real time. Velocity field of oxide smoke was solved by equilibrium Eulerian approximation. Then the velocity filed was used to solve an advection diffusion equation describing concentration of the oxide smoke. Finally, numerical simulation was carried out on certain type of SRM by this computational framework. Correct flow structure was given by simulation result which shows correctness of the computational framework.
作者 范兵 关正西
机构地区 第二炮兵工程学院
出处 《弹箭与制导学报》 CSCD 北大核心 2008年第2期146-148,共3页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 固体火箭发动机 大涡模拟 多相流 湍流 solid rocket motor large eddy simulation multiphase flow turbulence
分类号 V435 [航空宇航科学与技术—航空宇航推进理论与工程]
  • 相关文献

参考文献6

  • 1王丽丽,李家春,谢正桐.不可压缩流体三维Rayleigh-Taylor不稳定性的大涡模拟[J].中国科学（A辑）,2002,32(2):158-169. 被引量：1
  • 2Soshi K,Kozo F.Computational study of a supersonic base flow using LES/RANS hybrid methodology[C]// 42nd AIAA Aerospace Sciences Meeting and Exhibit,Reno,Nevada,2004.
  • 3Yoshizawa A.Statistical theory for compressible turbulent shear flows,with the application to subgrid modeling[J].Phys.Fluids,1986(29):2152-2164.
  • 4Wasistho B,Haselbacher A,Najjar F M,Tafti D,Balachandar S,et al.Direct and large eddy simulation of compressible wall-injection flows in laminar,transitional,and turbulent regimes[C]// 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,Indianapolis,2002.
  • 5Vreman A W.Direct and large-eddy simulation of the compressible turbulent mixing layer[D].Ph.D.Dissertation,University of Twente,1995.
  • 6Ferry J,Balachander S.A fast eulerian method for disperse two-phase flow[J].Int.J.Multiphase Flow,2001(27):1199-1226.

二级参考文献20

  • 1Sharp D H. An overview of Rayleigh-Taylor instability. Physica D, 1984, 12: 3～18
  • 2Baker G R, Meiron D I, Orszag S A. Vortex simulation of the Rayleigh-Taylor instability. Phys Fluids, 1980, 23: 1485～1490
  • 3Tryggvason G. Numerical simulations of the Rayleigh-Taylor instability. J Comput Phys 1988, 75: 253～282
  • 4Mulder W, Osher S, Sethian J. Computing interface motion in compressible gas dynamics. J Comput Phys, 1992, 100: 209～228
  • 5Osher S, Sethian J. Fronts propagating with curvature-dependent speed: algorithms based on Hamilton-Jacobi formulations. J Comput Phys, 1988, 79(1): 12～49
  • 6Li X L. Study of three-dimension-dimensional Rayleigh-Taylor instability in compressible fluids through level set method and parallel computation. Phys Fluids, 1993, 5(8): 1904～1913
  • 7Li X L, Jin B X, Glimm J. Numerical study for the three-dimensional Rayleigh-Taylor instability through the TVD/AC scheme and parallel computation. J Comput Phys, 1996, 126: 343～355
  • 8Holmes R L, Grove J W, Sharp D H. Numerical investigation of Richtmyer-Meshkov instability using front tracking. J Fluid Mech, 1995, 301: 51～64
  • 9Gardner C, Glimm J, McBryan O, et al. The dynamics of bubble growth for Rayleigh-Taylor unstable interfaces. Phys Fluids, 1988, 31: 447～465
  • 10He X Y, Chen S Y, Zhang R Y. A lattice Boltzmann scheme for incompressible multiphase flow and its application in simulation of Rayleigh-Taylor instability. J Comput Phys, 1999, 152: 642～663
弹箭与制导学报
2008年 第2期

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