首页|近壁旋转圆柱流场特性数值模拟分析

近壁旋转圆柱流场特性数值模拟分析

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[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.
Numerical simulation analysis of flow around near-wall rotating cylinder
[Objectives]To investigate the near-wall rotating cylindrical wake and hydrodynamic character-istics,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 Reyn-olds number Re=200 was carried out to compare the cylindrical wake and hydrodynamic characteristics at dif-ferent 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-pat-tern 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 amp-litude is increasing significantly;at higher reverse rotation rates,the cylindrical surface is wrapped by a posit-ive 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.

flow around cylinderrotatingnear-wall cylinderlift and drag forcevortex layer separation

王宗鹏、刘炳文、包燕旭、陈威、唐国强、李晓彬

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武汉理工大学 理学院,湖北 武汉 430063

武汉理工大学 船海与能源动力工程学院,湖北 武汉 430063

大连理工大学 海岸和近海工程国家重点实验室,辽宁 大连 116024

圆柱绕流 旋转 近壁圆柱 升阻力 涡层分离

国家自然科学基金湖北省自然科学基金大连理工大学海岸和近海工程国家重点实验室开放基金

522013342021CFB064LP2203

2024

中国舰船研究
中国舰船研究设计中心

中国舰船研究

CSTPCD北大核心
影响因子:0.496
ISSN:1673-3185
年,卷(期):2024.19(2)
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