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本文报道了微重力条件下90°弯管内气液两相流型实验结果。弯管内径12.7 mm,弯曲半径76.5mm,气、 液两相表观流速分别为1.0—23.6 m/s和0.09—0.5 m/s。本文分析了观测到的弹状流、弹-环过渡流和环状流的典型特 征,比较了与微重力直管内相应流型间及常重力弯管两相流型间的异同。 相似文献
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对水力直径为2.5 mm的正方形小通道内的非牛顿流体-氮气的垂直向上两相流动流型进行了可视化实验,工质分别为:浓度0.2%的聚丙烯酰胺(PAM)和0.2%的黄原胶(XG)水溶液,表观气速0.1~100 m/s,表观液速0.01~6 m/s.观察到的典型流型有:弹状流、搅拌流、弹环状流和环状流,其中弹环状流未见于水-空气上升流动.在PAM-氮气实验中发现了一种新流型-泡状-弹状流.通过流型图对比,发现非牛顿流体的搅拌流区域较牛顿流体窄,弹状-搅拌流转变线也明显右移,非牛顿流体的黏性对流型转变的影响较大. 相似文献
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利用气液两相流电导波动信号构建了流型复杂网络. 基于K均值聚类的社团探寻算法对该网络的社团结构进行了分析,发现该网络存在分别对应于泡状流、段塞流及混状流的三个社团,并且两个社团间联系紧密的点分别对应于相应的过渡流型. 基于复杂网络理论从全新的角度探讨了两相流流型复杂网络社团结构及统计特性问题,并取得了满意的流型识别效果,与此同时,在对该网络特性进一步分析的基础上,发现了对两相流流动参数变化敏感的相关复杂网络统计量,为更好地理解两相流流型动力学特性提供了参考.
关键词:
两相流流型
复杂网络
社团探寻算法
网络统计特性 相似文献
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利用有机玻璃管、吸管、泡沫球等简易材料自制了演示流体压强与流速关系的实验装置。该装置有效地解决了小球随意滚动、吹气方向不固定等问题。实验用泡沫球代替乒乓球,并将其放置在玻璃管中放置,使实验过程不受外界空气影响,且较轻的泡沫球更易运动,实验效果更明显。利用该原理还自制了模拟非洲草原犬鼠洞穴的演示装置,有趣且直观地演示了犬鼠洞穴中的气体流向。 相似文献
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1引言圆柱绕流是流动与传热领域的基本流动现象,也是历史悠久的研究课题。“经过多年的努力,人们已经获得了圆柱绕流的基本图象,积累了相当丰富的实验及分析资料,但有许多问题至今仍然是不解之谜[1]。在这些问题中,亚临界绕流时的绕流阻力具有重要的意义。在能源、化工、环保等工业领域大量存在的圆管外绕流,其绕流雷诺数大多在104数量级,为典型的亚临界绕流工况。在该雷诺数范围内,圆柱绕流阻力系数Cd≈1.2,处于较高水平。降低亚临界绕流圆柱的流动阻力将产生工业上量大面广的节能效益。为探索实用的流动减阻技术,必须对亚临界… 相似文献
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A mathematical model was developed to simulate two-phase gas-dispersed flow moving through a pipe with axisymmetric sudden
expansion. In the model, the two-fluid Euler approach was used. The model is based on solving Reynolds-averaged Navier — Stokes
equations for a two-phase stream. In calculating the fluctuating characteristics of the dispersed phase, equations borrowed
from the models by Simonin (1991), Zaichik et al. (1994), and Derevich (2002) were used. Results of a comparative analysis
with previously reported experimental and numerical data on two-phase flows with separation past sudden expansion in a plane
channel and in a pipe are given.
This work was supported by the President of the Russian Federation through the Foundation for Young Candidates of Sciences
under Grant MK-186.2007.8 and by the Russian Foundation for Basic Research (Grants Nos. 05-08-33586 and 06-08-00967). 相似文献
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在Ma=3.0的超声速风洞中, 分别对上游边界层为超声速层流和湍流, 压缩角度为25°和28°的压缩拐角流动进行了实验研究. 采用纳米粒子示踪平面激光散射(NPLS)技术获得了流场整体和局部区域的精细结构, 边界层、剪切层、分离激波、回流区和再附激波等典型结构清晰可见, 测量了超声速层流压缩拐角壁面的压力系数. 从时间平均的流场结构中测量出分离激波、再附激波的角度和再附后重新发展的边界层的增长情况, 通过分析时间相关的流场NPLS图像, 可以发现流场结构随时间的演化特性. 实验结果表明: 在25°的压缩角度下, 超声速层流压缩拐角流动发生了典型的分离, 边界层迅速增长失稳转捩, 并引起一道诱导激波, 流场中出现了K-H涡、剪切层和微弱压缩波结构, 而超声速湍流压缩拐角流动没有出现分离, 湍流边界层始终表现为附着状态; 在28° 的压缩角度下, 超声速层流压缩拐角流动进一步分离, 回流区范围明显扩大, 诱导激波、分离激波向上游移动, 再附激波向下游移动, 分离区流动结构复杂, 相比之下, 超声速湍流压缩拐角流动的回流区范围明显较小, 边界层增长缓慢, 流场中没有出现诱导激波、K-H涡和压缩波, 流动分离区域的结构也相对简单, 但分离激波的强度则明显更强.
关键词:
压缩拐角
层流
湍流
流动结构 相似文献
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Langevin simulations are preformed on the depinning dynamics of fluid monolayer on a quenched substrate. With increase in the strength of the substrate, we find for the first time a crossover from elastic crystal to smectic flows as well as a crossover from smectic to plastic flows above the depinning. A power-law scaling relationship can be derived between the drift velocity and the driving force for both the elastic crystal and smectic flows, but fails to be obtained for the plastic flow. The power-law exponents are found to be no larger than 1 for the elastic crystal flow and larger than 1 for the smeetic flow. The critical driving force and the averaged intensity of Bragg peaks remain invariant basically in the regime of smectic flow. A sudden increase in the critical driving force is observed within the crossover from the smeetic to plastic flows, and the averaged intensity of Bragg peaks shows sudden decreases within the crossovers both from the elastic crystal to smectic flows and from the smectic to plastic flows. The results are helpful for understanding the slip dynamics of fluids on a molecular level. 相似文献
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Langevin simulations are preformed on the depinning dynamics of fluidmonolayer on a quenched substrate. With increase in the strength of thesubstrate, we find for the first time a crossover from elastic crystal tosmectic flows as well as a crossover from smectic to plastic flows above thedepinning. A power-law scaling relationship can be derived between the driftvelocity and the driving force for both the elastic crystal and smecticflows, but fails to be obtained for the plastic flow. The power-lawexponents are found to be no larger than 1 for the elastic crystal flow andlarger than 1 for the smectic flow. The critical driving force and theaveraged intensity of Bragg peaks remain invariant basically in the regimeof smectic flow. A sudden increase in the critical driving force is observedwithin the crossover from the smectic to plastic flows, and the averagedintensity of Bragg peaks shows sudden decreases within the crossovers bothfrom the elastic crystal to smectic flows and from the smectic to plastic flows.The results are helpful for understanding the slip dynamics of fluids on a molecular level. 相似文献
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以Taitel 和Barnea(1998,1999)提出的段塞流跟踪模型为基础,进一步考虑加速压降的影响,建立了新的瞬态段塞流跟踪模型,并采用面向对象技术编制了数值模拟软件,实现了数值跟踪。计算结果与King等的段塞流气体流量瞬变实验数据对比表明,瞬态跟踪模型较好地预测了气体流量上升造成的段塞流压力“过升”现象,以及长液塞的出现;当气体流量下降时出现的压力“过降”现象和短暂分层流现象也由模型准确预测,分析认为,由于段塞流压降远高于分层流型,因此大部分液塞消失而出现的短暂分层流导致了压力过降。 相似文献