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首页> 外文期刊>Journal of Fluid Mechanics >THREE-DIMENSIONALLY PERTURBED VORTEX TUBES IN A ROTATING FLOW
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THREE-DIMENSIONALLY PERTURBED VORTEX TUBES IN A ROTATING FLOW

机译:旋转流中的三维扰动涡流管

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Numerical experiments are used to study the evolution of perturbed vortex tubes in a rotating environment in order to better understand the process of two-dimensionalization of unsteady rotating flows. We specifically consider non-axisymmetric perturbations to columnar vortices aligned along the axis of rotation. The basic unperturbed vortex is chosen to have a Gaussian cross-sectional vorticity distribution. The experiments cover a parameter space in which both the strength of the initial perturbation and the Rossby number are varied. The Rossby number is defined here as the ratio of the maximum amplitude of vorticity in the Gaussian vorticity profile to twice the ambient rotation rate. For small perturbations and small Rossby numbers, both cyclones and anticyclones behave similarly, relaxing rapidly back toward two-dimensional columnar vortices. For large perturbations and small Rossby numbers, a rapid instability occurs for both cyclones and anticyclones in which antiparallel vorticity is created. The tubes break up and then re-form again into columnar vortices parallel to the rotation axis (i.e. into a quasi-two-dimensional flow) through nonlinear processes. For Rossby numbers greater than 1, even small perturbations result in the complete breakdown of the anticyclonic vortex through centrifugal instability, while cyclones remain stable. For a range of Rossby numbers greater than 1, after the breakdown of the anticyclone, a new weaker anticyclone forms, with a small-scale background vorticity of spectral shape given approximately by the -5/3 energy spectral law. [References: 45]
机译:数值实验用于研究旋转环境中扰动涡旋管的演化,以便更好地理解非定常旋转流的二维过程。我们专门考虑对沿旋转轴对齐的圆柱状涡流的非轴对称扰动。选择基本无扰动涡流以使其具有高斯截面涡流分布。实验覆盖了一个参数空间,其中初始扰动的强度和Rossby数均发生变化。罗斯比数在这里定义为高斯涡度曲线中最大涡度与环境转速的两倍之比。对于较小的扰动和较小的Rossby数,旋风分离器和反旋风分离器的行为类似,迅速向二维柱状涡旋回驰。对于较大的扰动和较小的Rossby数,在旋风分离器和反旋风分离器中均会发生快速不稳定性,其中会产生反平行涡度。这些管破裂,然后通过非线性过程再次形成平行于旋转轴的圆柱状涡流(即准二维流)。对于大于1的Rossby数,即使很小的扰动也会通过离心不稳定性导致反气旋涡旋完全破裂,而旋风分离器保持稳定。对于大于1的Rossby数范围,在反气旋分解后,会形成一个新的较弱的反气旋,其频谱形状的小规模背景涡旋大约由-5/3能谱定律给出。 [参考:45]

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