共查询到20条相似文献,搜索用时 265 毫秒
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《工程热物理学报》2010,(6)
本文重点研究了微通道内入口效应和粗糙度等因素对流动阻力特性的影响。实验结果表明;对于粗糙度3.5%,水力直径为345μm的微圆管,入口段长度比常规管道短,转捩雷诺数Re_c位于2000~2300,其内入口效应并不影响微管内流体从层流到湍流转捩的拐点位置;内径为112.6μm和169.8μm,高宽比为0.59和0.63以及粗糙分别为1.29%和2.03%的矩形微通道内流动由层流向湍流的转捩发生在Re≈1600~2800之间。实验结果表明,微尺度是微管内流体转捩提前的必要条件,但不是充分条件,拐点提前是由多因素综合作用所造成的结果,其机理有待于进一步研究。 相似文献
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逆压梯度下层流分离泡转捩的大涡模拟 总被引:7,自引:1,他引:6
本文采用有限体积法,发展了适合复杂几何边界条件的可压缩流动大涡模拟程序,通过对槽道湍流的计算,验证了程序的可靠性。对低雷诺数、逆压梯度环境中的层流分离泡转捩现象进行了数值模拟,分析了其统计特性及大尺度相干结构的演化规律.初步的结果表明:大涡模拟可以很好地处理层流分离泡转捩问题,既能给出满意的统计平均结果,又可以通过相干结构的演化细致描述分离泡转捩的动力学过程。 相似文献
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滑移流区内微环缝槽道中的层流流动与换热 总被引:7,自引:0,他引:7
本文针对微环缝槽道采用速度滑移和温度跳跃边界条件求解了不可压缩气体的N-S方程和能量方程,理论分析了微环缝槽道在单侧或双侧不同热流密度加热条件下的流动与层流换热特性,讨论了Kn数、内外径比对流动阻力及换热特性的影响。结果表明:滑移流区微环继通道内的流阻和Nusselt数明显低于连续流区;且随着Kn数的增加,流阻和Nusselt数均减小;但其随内外径比r*的变化趋势与连续流区相似。 相似文献
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《物理学报》2016,(19)
为了探讨槽道中纤维悬浮湍流场特性,本文对修正的雷诺平均纳维-斯托克斯方程、含纤维项的湍动能和耗散率方程、纤维动力学方程以及纤维取向概率密度函数方程进行了数值研究,同时进行了相关实验以验证计算结果.研究结果表明,流场中尤其是近壁区域,纤维取向趋向于与流动方向一致,且该现象随着雷诺数和纤维浓度的减小以及纤维长径比的增大而更为明显.纤维在槽道中分布不均匀,但随着雷诺数的增大和纤维长径比的减小趋于均匀.相对于单相流,纤维悬浮流的流向平均速度剖面更陡峭,且剖面斜率随着纤维浓度、长径比的增大以及雷诺数的减小而变大,纤维的存在使湍流场的湍动能和雷诺应力减小,且减小程度随着纤维浓度和长径比的增大以及雷诺数的减小而增加.流场中的第一法向应力差小于0.05且远小于剪切应力.从壁面到中心,剪切应力增加而第一法向应力差减小.剪切应力和第一法向应力差都随着纤维浓度和长径比的增大而增大.随着雷诺数的增大,剪切应力增大而第一法向应力差减小.纤维浓度对于剪切应力和第一法向应力差的影响比纤维长径比更显著. 相似文献
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层流叶片在压气机中的应用研究 总被引:1,自引:0,他引:1
《工程热物理学报》2017,(11)
压气机叶片表面层流流动及转捩现象的捕捉是研究压气机层流叶型的重点和关键。通过基于SST转捩模型的数值方法对某压气机叶型进行数值模拟分析,以精确捕捉普通湍流模型无法捕捉的叶片表面的层流流动及转捩现象,并给定叶片表面转捩的判定依据。在此基础上深入研究低雷诺数环境和高湍流度环境对压气机叶片表面层流流动的影响,验证了在实际压气机环境下,叶片表面的层流流动是可能存在的。为后续压气机层流叶型设计提供数值验证手段和可行性验证基础。 相似文献
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为满足固体激光器用微通道冷却器的换热要求, 根据冷却器结构分别建立了二维和三维物理模型, 利用计算流体力学方法首先对比研究两者的流动特性, 然后考察雷诺数和玻片生热量对微通道流动和传热特性的影响。结果表明:对于类似大平板间的矩形微通道层流流动区域, 其流动及传热特性可直接采用二维简化模型进行模拟分析;对于重点关注的转捩区, 采用三维模型模拟分析更好;当雷诺数增大到转捩点, 流体的传热效果得到明显增强;随着雷诺数的增大, 玻片生热量对通道内最低压力需求的影响逐渐减小;不同玻片生热量对微通道流动影响不可忽略, 对努赛尔数和通道总压降基本无影响。 相似文献
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展向旋转槽道湍流中的标量场输运过程是与众多工程流动直接相关的模型问题。基于直接数值模拟工作对该问题开展系统性的研究。由壁面摩擦速度定义的流动Reynolds数固定在180,重点考察Schmidt数和旋转数的影响。结果表明,较弱旋转强度即可对主导流动结构形态产生明显的影响:此时槽道不稳定侧产生流向大尺度结构,由此导致标量场出现条带状结构。强旋转时不稳定侧出现被湍流充分混合的区域,而在稳定侧流动层流化并出现近似传导区。平均标量剖面在湍流区和层流区呈现斜率不同的线性分布。Schmidt数小于1时,湍流区标量场脉动和湍流输运随旋转数出现非单调变化,而Schmidt数大于等于1时两者都随旋转数单调下降。由此导致总标量传输率在Schmidt数小于1时随旋转数先上升后下降,而当Schmidt数大于1时单调下降且在弱旋转区域下降趋势最快。 相似文献
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微柱群阻力特性实验研究 总被引:1,自引:0,他引:1
以去离子水为工质,流经直径为0.5 aim,高度分别为1.0 mm、0.75 mm、0.5 mm和0.25 mm的圆柱组成的柱群板,其宽度与长宽分别为3.5 mm和40 mm,测量通道进出口压差及流量,研究微柱群内部分别在叉排和顺排时液体流动的阻力特性.研究表明,微柱群内流动阻力系数f,随Re数的增大而逐渐减小,当Re数大于500时,f基本不变;微柱高度和直径之间存在一个有利于流动的最佳比例,该值介于1到1.5之间;顺排微柱群的f明显小于叉排微柱群,其,值为叉排微柱群的0.5倍. 相似文献
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Experiments were conducted to investigate the flow characteristics of water flowing through rectangular microchannels having hydraulic diameters of 0.133-0.367 mm and H/W ratios of 0.333-1. Experimental results indicated that the laminar flow transition occurred at Reynolds numbers of 200-700. This critical Re for the laminar transition was strongly affected by the hydraulic diameter, decreasing with corresponding decreases in the microchannel. In addition, the size of the transition range was diminished and fully developed turbulent flow also occurred at much lower Re. The friction behavior of both the laminar and turbulent flow was found to depart from the classical thermqfluid correlations. lite friction factor, f, was found to be proportional to Re?1.98 rather than Re for the laminar condition, and proportional to Re?1.72i for turbulent flow. The geometric parameters, hydraulic diameter, and H/W were found to be the most important parameters and had a critical effect on the flow. Generally, increasing the ratio H/W increases the friction factor. The reduction of the microchannel hydraulic radius decreases the friction factor significantly for a given H/W. There exists a special range of ratio H/W (approximately 0.5 mm) at which the experimental data are lower than the predictions obtained from classical correlations. Continued reduction of channel size increases the difference between fI,expf1,theo at REcri, and the quantity of fI,exp becomes smaller within the region adjacent to H/W = 0.5, and larger when H /Wis out of this region. 相似文献
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以水气两相流为研究对象, 采用大涡模拟和流体体积法, 结合破碎准则和第三代涡识别方法对双气泡碰撞过程进行数值模拟。采用单一变量法, 研究气泡直径比、相对偏心距及气泡间相对距离对气泡破碎程度的影响。双气泡碰撞过程中, 两气泡的直径越接近时, 碰撞过程中的气泡破碎程度越弱, 偏心距的变化对气泡破碎程度影响不大。而相对距离小于1时, 随着其增大, 气泡碰撞过程中的破碎程度更加明显。当气泡相对距离大于1时, 气泡破碎程度趋于平缓。研究表明: 第三代涡识别方法能够很好地捕捉两相流湍流流场中漩涡位置, 并能敏锐地反映出湍流的变化。 相似文献
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Experimental investigations had been conducted to study the forced convective heat transfer and pressure drop characteristics of the hydrodynamic fully developed turbulent flow in horizontal equilateral triangular ducts fabricated with Ike same length and hydraulic diameter but different surface roughness of 1.2, 3.0, and 11.5 μm. The experiments were performed with hydraulic diameter-based Reynolds number ranging from 7,000 to 20,000. The entire inner wall of the duct was heated uniformly, while the outer surface was thermally insulated. It was found that the variation of Stanton number (St) with friction factor (f) can be expressed by a relationship of St = C * f, where the constant (C) increases from 0.41 to 0.50 when the surface roughness is increased from 1,2 to 11.5 μm. It was also concluded that the duct with a higher surface roughness will have better heat transfer performance. Nondimensional expressions for the determination of the heat transfer coefficient and friction factor of the equilateral triangular ducts with different surface roughness were also developed. 相似文献
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《等离子体物理论文集》2017,57(2):58-66
Plasma jets from conventional non‐transferred arc plasma devices are usually operated in turbulent flows at atmospheric pressure. In this paper, a novel non‐transferred arc plasma device with multiple cathodes is introduced to produce long, laminar plasma jets at atmospheric pressure. A pure helium atmosphere is used to produce a laminar plasma jet with a maximum length of >60 cm. The influence of gas components, arc currents, anode nozzle diameter, and gas flow rate on the jet characteristics is experimentally studied. The results reveal that the length of the plasma jet increases with increasing helium content and arc current but decreases with increasing nozzle diameter. As the gas flow rate increases, the length of the plasma jet initially increases and then decreases. Accordingly, the plasma jet is transformed from a laminar state to a transitional state and finally to a turbulent state. Furthermore, the anode arc root behaviours corresponding to different plasma jet flows are studied. In conclusion, the multiple stationary arc roots that exist on the anode just inside the nozzle entrance are favourable for the generation of a laminar plasma jet in this device. 相似文献
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This article presents an investigation on heat transfer enhancement in a round tube inserted with a helically twisted tape. The effects of a helically twisted tape with alternate axis (HTT-A) on heat transfer, friction factor, and thermal performance factor behaviours are reported for the turbulent regime. HTT-A geometries are tape pitch to tube diameter, P/D = 1.0, 1.5, and 2.0; alternate length to pitch length, l/P = 1.0, 1.5, and 2.0; twisted length to tape width, y/W = 3.0; and tape width to tube diameter, w/D = 0.2. The experiment has been performed by varying the volumetric air flow rate in order to adjust Reynolds number ranging from 6 000 to 20 000. The wall of the testing tube is uniformly heated as a constant heat flux while the tests are covered with thermal insulations to reduce heat loss to surroundings. Thermal performance is evaluated by comparing the present experimental results with the results of the modified HTT-A and also those obtained from previous study (conventional helically twisted tape, HTT). The thermal performance of tested tube with HTT-A is evaluated to obtain the degree of heat transfer enhancement and friction factor induced by HTT-A with respect to the plain tube under the same test conditions. Evenly, it is interesting to observe that the tube with HTT-A consistently possesses higher heat transfer and thermal performance factor than those with the HTT around 14.1% and 1.9%, respectively. The HTT-A with the smaller pitch ratio and adjacent twist length provides higher heat transfer rate and friction factor than the one with larger pitch ratio and alternate length as a result of a larger contact surface area, stronger swirl intensity and, thus, better fluid mixing near the tube wall. In the range determined, the tubes with the largest pitch ratio (P/D = 2.0) and smallest alternate length (l/P = 1.0) give the highest thermal performance factor at around 1.35. In addition, the empirical correlations of the Nusselt number, friction factor, and thermal performance factor are also described. 相似文献
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V. P. Vorotilin 《Journal of Experimental and Theoretical Physics》2018,126(2):262-275
The problem of flow and combustion of turbulent jets of fuel gas in the external medium of an oxidant (air) is solved with regard to the existence of the actual boundary of the turbulent flow region of a jet. Based on the ideas of the friction force of the external flow acting on the boundary of a jet, the entrainment equation for the external medium is derived that closes the system of equations of motion of turbulent jets. The physical meaning of the dissipation rate of the turbulent energy of a jet is interpreted as the work of the friction force. To describe the combustion kinetics, the limit of instantaneous reactions corresponding to the diffusion combustion mode is used. Calculations of the effective reaction rates for reactants and the volumes occupied by them are based on the representation of a turbulent medium as an aggregation of independent turbulent particles—vortices—whose random contacts lead to the mixing and combustion of reacting substances [31]. The concomitant phenomena of flow and combustion are analyzed, including radiation effects. In particular, it is shown that the apparent increase in the combustion temperature with increasing Reynolds number is in fact attributed to the relative decrease of thermal radiation losses. Qualitative agreement is obtained between the results of the theoretical calculations of the length of a combustion torch and experimental data. 相似文献