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运动物体与运动激波干扰流场特性数值研究 被引量:2

Computational analysis of the unsteady flow induced by the interference between a moving body and a moving shock wave
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摘要 用数值方法求解非定常可压缩Navier-Stokes方程,模拟了运动物体分别以超声速和亚声速穿越激波的全过程。在这两种情况下,激波都是从高压区运动到低压区,阻力急剧地减小,但在亚声速情况下,会在物体上产生不对称力和力矩,导致运动物体的不稳定。 The numerical simulations of the flow field around double-wedge shaped projectile overtaking shocks are carried out by solving the unsteady compressible Navier-Stokes equations. Two test cases of the supersonic overtaking and the subsonic overtaking are considered. A rapid reduction of the drag force is observed in both cases as the projectile moves from the high pressure region to the low pressure region. The strong asymmetric force and torque that may create an unstable projectile motion are observed only in the case of the subsonic.
出处 《计算力学学报》 EI CAS CSCD 北大核心 2003年第3期346-349,371,共5页 Chinese Journal of Computational Mechanics
基金 国防科技预研基金(00J13.2.1.HT7102)资助项目.
关键词 运动物体 非定常流 数值模拟 超声速穿越 亚声速穿越 激波干扰 流场特性 Computer simulation Flow of fluids Navier Stokes equations Shock waves Subsonic flow Supersonic flow
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参考文献3

  • 1江娟,周伟江.二维双楔外形穿越激波流场特性及其数值分析[J].空气动力学学报,2002,20(3):260-266. 被引量:3
  • 2Glaz H M, Colclla P, Glass I I, et al. A Detailed Numerical, Graphical and Experimental Study of Oblique Shock Wave Reflections [R]. Lawrence Berkeley Laboratory Report LBL-20033, April,1985.
  • 3Watanable R, Fujii K, et al. Computational analysis of the unsteady flow induced by a projectile overtaking a preceding shock wave[J]. Trans Japan Soc Aero Space Sci,1998,41(132):65-73.

二级参考文献3

  • 1[1]傅德薰,汪翼云,马延文.计算空气动力学[M].1994,宇航出版社.
  • 2[2]WATANABLE R,FUJII K et.al. Computational analysis of the unsteady flow induced by a projectile overtaking a preceding shock wave[J]. Trans Japan Soc Aero. space Sci.,1998,41(132):65-73.
  • 3[3]GLAZ H M, COLCLLA P, GLASS I I and DESCHAMBAULT R L. A detailed numerical, graphical and experimental study of oblique shock wave reflections[R]. Lawrence Berkeley Laboratory Report LBL-20033, April, 1985.

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