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浮力对混合对流流动及换热特性的影响 被引量:4
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作者 刘明侯 t.l.chan 陈义良 《力学学报》 EI CSCD 北大核心 2004年第3期336-341,共6页
用热线和冷线相结合的技术测量垂直圆管内逆混合对流流体的平均速度、温度以及它们的脉动.较详细地研究了浮力对逆混合对流的流动特性和传热特性的影响.评估了实验中采用的冷线测量温度补偿速度探头温度敏感的影响.逆混合对流的传热结... 用热线和冷线相结合的技术测量垂直圆管内逆混合对流流体的平均速度、温度以及它们的脉动.较详细地研究了浮力对逆混合对流的流动特性和传热特性的影响.评估了实验中采用的冷线测量温度补偿速度探头温度敏感的影响.逆混合对流的传热结果用无量纲参数Ω(Ω=Grd/Re2d)来表示,其中,基于管道直径的雷诺数Rea变化范围为900-18000,浮力参数Ω变化范围为0.004 899-0.504 7.研究结果表明,浮力对逆混合对流的换热有强化作用.随着葛拉晓夫数Grd的增加,温度脉动,流向雷诺正应力和流向温度通量增大,并且在靠近壁面的流体区域尤其明显.热线与冷线相结合的技术适合于研究非绝热的流动测量,可以用于研究浮力对流动和换热特性的影响. 展开更多
关键词 传热学 混合对流 浮力 雷诺数 浮力参数
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狭缝射流撞击圆柱表面的湍流特性实验研究 被引量:3
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作者 刘明侯 t.l.chan 《力学学报》 EI CSCD 北大核心 2005年第2期135-140,共6页
实验研究了狭缝射流撞击圆柱表面后壁面射流区的平均流动和湍流特性.考察了雷诺数Re(6000~20000),喷口到受撞表面距离Y/W(5~13),喷口宽度W(6.25mm,9.38mm),受撞表面曲率(半圆柱体直径D=150mm)对流动和湍流结构的影响.通过分析X热线在... 实验研究了狭缝射流撞击圆柱表面后壁面射流区的平均流动和湍流特性.考察了雷诺数Re(6000~20000),喷口到受撞表面距离Y/W(5~13),喷口宽度W(6.25mm,9.38mm),受撞表面曲率(半圆柱体直径D=150mm)对流动和湍流结构的影响.通过分析X热线在壁面射流区的测量结果发现,在近壁区域,表面曲率、Rew,Y/W和S/W等参数对√u2/Um的影响比对√-v2/Um强,并且切应力-uv/U2m对表面曲率变化最敏感.当喷口与受撞击表面之间的距离Y/W在一定范围内增加时,沿圆柱表面流动的流向和横向的湍流强度增强.用平板射流和圆柱体表面壁面射流的数据进行比较,从而得到表面曲率对壁面射流特性的影响.结果表明,曲率对壁面射流的影响较强,并随着S/W的增大而增强.随着雷诺数的增大,壁面曲率的影响也有强化的趋势. 展开更多
关键词 狭缝射流 曲率影响 湍流特性 壁面射流 半圆柱表面
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Flow instability of nanofuilds in jet
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作者 Yi XIA Jianzhong LIN +1 位作者 Fubing BAO t.l.chan 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2015年第2期141-152,共12页
The flow instability of nanofluids in a jet is studied numerically under various shape factors of the velocity profile, Reynolds numbers, nanoparticle mass loadings,Knudsen numbers, and Stokes numbers. The numerical r... The flow instability of nanofluids in a jet is studied numerically under various shape factors of the velocity profile, Reynolds numbers, nanoparticle mass loadings,Knudsen numbers, and Stokes numbers. The numerical results are compared with the available theoretical results for validation. The results show that the presence of nanoparticles enhances the flow stability, and there exists a critical particle mass loading beyond which the flow is stable. As the shape factor of the velocity profile and the Reynolds number increase, the flow becomes more unstable. However, the flow becomes more stable with the increase of the particle mass loading. The wavenumber corresponding to the maximum of wave amplification becomes large with the increase of the shape factor of the velocity profile, and with the decrease of the particle mass loading and the Reynolds number. The variations of wave amplification with the Stokes number and the Knudsen number are not monotonic increasing or decreasing, and there exists a critical Stokes number and a Knudsen number with which the flow is relatively stable and most unstable,respectively, when other parameters remain unchanged. The perturbation with the first azimuthal mode makes the flow unstable more easily than that with the axisymmetric azimuthal mode. The wavenumbers corresponding to the maximum of wave amplification are more concentrated for the perturbation with the axisymmetric azimuthal mode. 展开更多
关键词 nanoparticle-laden jet flow hydrodynamic instability Stokes number Knudsen number particle mass loading
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