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首页> 外文期刊>Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering >Direct numerical simulation of the transitional separated fluid flows around a sphere and a circular cylinder
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Direct numerical simulation of the transitional separated fluid flows around a sphere and a circular cylinder

机译:过渡分离流体绕球体和圆柱体流动的直接数值模拟

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For the investigation of transitional (from 2D to 3D unsteady) regimes of separated fluid flows around a sphere and a circular cylinder the direct numerical simulation is used. Transitional (from 2D axisymmetrical to 3D unsteady) regimes for a sphere were obtained for 210.5 ≤ Re ≤603. For 210.5 ≤ Re ≤ 297 the flow is steady but not axisymmetrical with non-zero lift/side and torque moment coefficients (the so-called double-thread wake). For 298 ≤ Re ≤ 603 the flow is unsteady and periodical but again with non-zero time-averaged lift/side and torque moment coefficients. Only for Re ≥ 604 these time-averaged coefficients are equal to zero. The calculated vortex structure of the wake is successfully used for flow visualisation. An analysis of the dynamics of these structures for RE = 880 reveals a sequence of shed hairpin vortices in combination with a sequence of secondary vortex loops around the legs of the hairpin vortices. Transitional regimes of separated fluid flows around a circular cylinder were obtained for 200 ≤ Re ≤ 400. For 200 ≤ Re ≤ 300 obtained periodical 3D flows are corresponding to known mode A (with periodical structures along the axis of a cylinder equal to 3.5d ≤ λ ≤ 4d, where d is the diameter of the cylinder). The regime with large dislocations previously discovered in experiments was obtained numerically for 220 ≤ Re ≤ 260. For 300 ≤ Re ≤ 400 obtained periodical structures have length 0.8d ≤ λ ≤ 0.9d approximately, which is in agreement with known mode B. For Re = 300 obtained both modes A and B are existing simultaneously. The splitting on physical factors method for incompressible fluid flows (SMIF) with hybrid explicit finite difference scheme (second-order accuracy in space, minimum scheme viscosity and dispersion, capable of work in wide range of Reynolds numbers and monotonous) and O-type grids were used.
机译:为了研究分离的流体在球体和圆柱体周围的过渡(从2D到3D非稳态)状态,使用了直接数值模拟。对于210.5≤Re≤603,获得了球体的过渡(从2D轴对称到3D非稳态)状态。对于210.5≤Re≤297,流量是稳定的,但不是轴对称的,具有非零的升力/侧向和转矩力矩系数(所谓的双螺纹尾流)。对于298≤Re≤603,流量是不稳定的且周期性的,但时间/平均升力/侧向和转矩力矩系数也非零。仅当Re≥604时,这些时间平均系数才等于零。计算出的尾流涡流结构已成功用于流动可视化。对RE = 880的这些结构的动力学分析显示,一系列发夹形涡流与发夹形涡流腿周围的一系列次级涡流环组合在一起。对于200≤Re≤400,获得了绕圆柱体流动的分离流体的过渡状态。对于200≤Re≤300,获得的周期性3D流量对应于已知模式A(沿着圆柱轴的周期性结构等于3.5d≤ λ≤4d,其中d是圆柱体的直径)。对于220≤Re≤260,通过数值获得了先前在实验中发现的具有大位错的状态。对于300≤Re≤400,获得的周期性结构的长度大约为0.8d≤λ≤0.9d,这与已知的模式B一致。 = 300,同时存在模式A和B。混合显式有限差分方案(空间二阶精度,最小方案粘度和离散度,能够在广泛的雷诺数和单调范围内工作)的不可压缩流体流(SMIF)的物理因子分裂方法被使用。

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