王宗鹏, 刘炳文, 包燕旭, 等. 近壁旋转圆柱流场特性数值模拟分析[J]. 中国舰船研究, 2024, 19(2): 21–30. doi: 10.19693/j.issn.1673-3185.03194
引用本文: 王宗鹏, 刘炳文, 包燕旭, 等. 近壁旋转圆柱流场特性数值模拟分析[J]. 中国舰船研究, 2024, 19(2): 21–30. doi: 10.19693/j.issn.1673-3185.03194
WANG Z P, LIU B W, BAO Y X, et al. Numerical simulation analysis of flow around near-wall rotating cylinder[J]. Chinese Journal of Ship Research, 2024, 19(2): 21–30 (in both Chinese and English). doi: 10.19693/j.issn.1673-3185.03194
Citation: WANG Z P, LIU B W, BAO Y X, et al. Numerical simulation analysis of flow around near-wall rotating cylinder[J]. Chinese Journal of Ship Research, 2024, 19(2): 21–30 (in both Chinese and English). doi: 10.19693/j.issn.1673-3185.03194

近壁旋转圆柱流场特性数值模拟分析

Numerical simulation analysis of flow around near-wall rotating cylinder

  • 摘要:
    目的 为探讨近壁旋转圆柱尾流及流体力特性,对典型间隙比下旋转圆柱绕流进行研究。
    方法 对雷诺数Re = 200下3种典型间隙比(G/D = 0.2,0.8,1.4)的旋转圆柱绕流展开数值模拟,对比不同间隙比和转速比下的圆柱尾流及流体力特性。
    结果 结果显示:当G/D = 0.2时,圆柱表面脱涡会受到显著抑制,圆柱表面升阻力无波动;当G/D = 0.8和1.4且转速比较低时,会发生“尾流涡”脱落现象,其结构与2S模式相似,升阻力系数呈正弦周期性波动,振幅较小;当正旋转速较大时,圆柱表面无漩涡脱落,形成稳定的D模式尾流(随转速比增大由D+模式变为D模式),“尾流涡层”与“壁面涡层”发生分离,“壁面涡”呈现多周期性脱落现象,升阻力系数呈多周期波动,振幅显著增大;当反旋转速较大时,圆柱表面被一层正涡量的涡层包裹,漩涡脱落受到显著抑制,升阻力无波动。
    结论 所得结论可为高效流动控制技术发展提供参考。

     

    Abstract:
    Objectives To investigate the near-wall rotating cylindrical wake and hydrodynamic characteristics, flow around cylinder at typical gap ratios is investigated.
    Methods A numerical simulation of flow around a near-wall rotating cylinder with different gap ratios (G/D = 0.2, 0.8, 1.4) and rotation rates at Reynolds numberRe = 200 was carried out to compare the cylindrical wake and hydrodynamic characteristics at different gap ratios and rotation rates.
    Results The results show that: For G/D = 0.2, the cylindrical vortex shedding is significantly suppressed and the lift and drag force on the cylindrical surface remain steady. For G/D = 0.8 and G/D = 1.4, at low rotation rates, the "wake vortex" is shed and is similar to the 2S pattern, with sinusoidal periodic fluctuations in the lift and drag coefficients and small amplitude; at higher positive rotation rates, the cylindrical wake pattern is the stable D pattern with no vortex shedding (changing from D+ to D pattern as the rotation rate increases), the "wake vortex layer" is separated from the "wall vortex layer", the "wall vortex" is shed multi-periodically, the lift and drag coefficients are fluctuating multi-periodically and the amplitude is increasing significantly; at higher reverse rotation rates, the cylindrical surface is wrapped by a positive boundary layer, with no vortex shedding and no fluctuations in lift and drag.
    Conclusions The results can provide a reference for the development of high efficient flow control technology.

     

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