首页> 外文会议>Fourth Asia Workshop on Computational Fluid Dynamics(Fourth Japan-China Joint Workshop on CFD)(4AWCFD) >NUMERICAL SIMULATION ON A PLANAR SUPERSONIC FREE SHEAR LAYER WITH MIXING ENHANCEMENT
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NUMERICAL SIMULATION ON A PLANAR SUPERSONIC FREE SHEAR LAYER WITH MIXING ENHANCEMENT

机译:具有混合增强作用的平面超音速自由剪切层的数值模拟

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In the present study, direct numerical simulations have been carried out on a planar supersonic free shear flow at Mc=0.5. Navier-Stokes equations were solved with a finite difference method of third-order accuracy. At the first, the validation of computational grids was made, and the computational accuracy was investigated on different grid sizes by the linear mode of a 2-D parallel mixing layer. Then the DNS method was used to 3-D DNS computations with validated grid size. In the DNS study on a 3-D planar free shear layer with 2-D disturbing wave, it was found that a very week lateral wave was modulated naturally. By adding this 3-D wave at sub-harmonic frequency to the disturbing source of the primary wave, the instability process was enhanced greatly. It is noticeable that λ-structure of vortex developed, and the mixing enhancement can be achieved in this way. It is an important fact that distinguishable difference exists in supersonic shear layer between 2-D and 3-D considerations.
机译:在本研究中,直接数值模拟已在Mc = 0.5的平面超声速自由剪切流上进行。 Navier-Stokes方程用三阶精度的有限差分法求解。首先,对计算网格进行了验证,并通过二维并行混合层的线性模式研究了不同网格尺寸下的计算精度。然后将DNS方法用于经过验证的网格大小的3-D DNS计算。在具有2-D干扰波的3-D平面自由剪切层的DNS研究中,发现非常一周的侧向波是自然调制的。通过以次谐波频率将此3-D波添加到初级波的干扰源中,极大地增强了不稳定过程。值得注意的是,形成了涡旋的λ结构,并且可以以这种方式实现混合增强。一个重要的事实是,在超声波剪切层中,二维和三维考虑之间存在明显区别。

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