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刘旭亮, 张树海. 二维激波与剪切层相互作用的直接数值模拟研究[J]. 力学学报, 2013, 45(1): 61-75. DOI: 10.6052/0459-1879-12-106
引用本文: 刘旭亮, 张树海. 二维激波与剪切层相互作用的直接数值模拟研究[J]. 力学学报, 2013, 45(1): 61-75. DOI: 10.6052/0459-1879-12-106
Liu Xuliang, Zhang Shuhai. DIRECT NUMERICAL SIMULATION OF THE INTERACTION OF 2D SHOCKWAVE AND SHEAR LAYER[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(1): 61-75. DOI: 10.6052/0459-1879-12-106
Citation: Liu Xuliang, Zhang Shuhai. DIRECT NUMERICAL SIMULATION OF THE INTERACTION OF 2D SHOCKWAVE AND SHEAR LAYER[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(1): 61-75. DOI: 10.6052/0459-1879-12-106

二维激波与剪切层相互作用的直接数值模拟研究

DIRECT NUMERICAL SIMULATION OF THE INTERACTION OF 2D SHOCKWAVE AND SHEAR LAYER

  • 摘要: 采用五阶weighed esseritially non-oscillatory (WENO) 格式和三阶total variation diminishing (TVD) Runge-Kutta 格式, 通过求解二维非定常Navier-Stokes 方程, 直接数值模拟了激波与剪切层相互作用, 目的在于揭示激波与剪切层相互作用过程中噪声产生的机理. 研究发现:(1) 当入射激波穿过剪切层时, 剪切层中心位置向下层区域偏移;(2) 入射激波穿过剪切层产生小激波, 在小激波与剪切层接触点处产生声波并向外辐射;(3) 反射激波穿过剪切层后形成了分段弧状激波;(4) 当反射激波穿过剪切层时, 激波在鞍点处泄漏并向外辐射声波, 这是一种激波泄漏机制.

     

    Abstract: Direct numerical simulation (DNS) of the interaction of shock wave and shear layer was performed. The compressible unsteady two-dimensional Navier-Stokes equations were solved using the fifth-order WENO scheme combined with the third-order TVD Runge-Kutta scheme. The purpose of this paper is to reveal the mechanism of sound generation in the interaction of shock wave and shear layer. The results show that: (1) When incident shock wave is passing through the shear layer, the center of the vortex cores is shifted towards the lower side; (2) The interaction of incident shock wave and shear layer generates shocklet, and then acoustic wave is generated and radiated at the locus of contact of shocklet and shear layer; (3) Several arc-shocks are formed after reflected shock wave passing through shear layer; (4) When reflected shock wave is passing through shear layer, shock wave is leaking in the braid region and shock-associated noise is generated at the saddle points between vortices. This is a form of shock leakage mechanism.

     

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