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1.
Finite difference solution of the transient free-convection flow of an incompressible viscous fluid past an impulsively started
semi-infinite vertical plate with heat and mass transfer is presented here. The steady state velocity, temperature and concentration
profiles are shown graphically. Velocity profiles are compared with exact solution. It has been observed that there is a rise
in the velocity due to the presence of a mass diffusion. An increase in Schmidt number, leads to a fall in the velocity. Stability
and the convergence of the finite difference scheme are established.
Received on 7 January 1998 相似文献
2.
The secondary vortex structure of an impingement jet system is enhanced by V-ribs on both the impingement and target plates. Numerical and experimental investigations are conducted to study the flow field and heat transfer resulting from V-rib turbulators in an impingement cooling configuration. Three different cases are tested: V-ribs on both the impingement and target plates (V-rib), V-ribs only on the impingement plate (V-rib-impingement) and V-ribs only on the target plate (V-rib-target). The experiment is carried out on a 9 by 9 inline impingement array test facility. For the transient measurements, narrow band thermochromic liquid crystals (TLC) and thermocouples are applied to obtain the local heat transfer distribution. Pressure taps are used to measure the pressure loss. The numerical simulation is carried out with ANSYS CFX 14, using a steady state Reynolds-Averaged Navier-Stokes (RANS) approach and the Shear Stress Transport (SST) turbulence model. All studies are done for a Reynolds number range of 15,000 to 35,000. There is a good overall agreement between the experimental and numerical results for the cases studied. The detailed flow field from the numerical simulation is used to understand and complement the phenomena observed in the experiment. The evaluation of the flow field confirms that the V-ribs enhance the secondary flow structure in the impingement system and induce a positive heat flux ratio compared to the baseline case. Both experimental and numerical results show a Nusselt number increase for the V-rib-impingement and V-rib configuration, with a highest Nusselt number ratio of 1.16. Notice that the experiment cannot take the rib part into account due to the invalid 1D semi-infinite wall assumption there, while the CFD simulation allows for the consideration of heat transfer on the rib surface and thus complements the heat flux data on the target plate. Depending on the configuration, the CFD simulation shows a heat flux ratio of 1.06–1.34. The pressure loss of the system is comparable to the case with a smooth impingement plate and a smooth target plate. 相似文献
3.
An experimental investigation was conducted to study the convective heat transfer rate from a wedge-shaped surface to a rectangular subsonic air jet impinging onto the apex of the wedge. The jet Reynolds number, nozzle-to-surface distance and the wedge angle were considered as the main parameters. Jet Reynolds number was ranged from 5,000 to 20,000 and two dimensionless nozzle-to-surface distances h/w?=?4 and 10 were examined. The apex angle of the wedge ranged from 30° to 180° where the latter case corresponds with that of a flat surface. Velocity profile and turbulence intensity were provided for free jet flow using hot wire anemometer. Local and average Nusselt numbers on the impinged surface are presented for all the configurations. Based on the results presented, the local Nusselt number at the stagnation region increases as the wedge angle is decreased but, it then decreases over the remaining area of the impinged surface. Average Nusselt number over the whole surface is maximum when the wedge angle is 180° (i.e. plane surface) for any jet and nozzle-to-surface configuration. 相似文献
4.
The present paper focuses on the analysis of unsteady flow and heat transfer regarding an axisymmetric impinging synthetic
jet on a constant heat flux disc. Synthetic jet is a zero net mass flux jet that provides an unsteady flow without any external
source of fluid. Present results are validated against the available experimental data showing that the SST/k − ω turbulence model is more accurate and reliable than the standard and low-Re k − ε models for predicting heat transfer from an impinging synthetic jet. It is found that the time-averaged Nusselt number
enhances as the nozzle-to-plate distance is increased. As the oscillation frequency in the range of 16–400 Hz is increased,
the heat transfer is enhanced. It is shown that the instantaneous Nu distribution along the wall is influenced mainly by the interaction of produced vortex ring and wall boundary layer. Also,
the fluctuation level of Nu decreases as the frequency is raised. 相似文献
5.
Mixed convection heat transfer about a semi-infinite inclined plate in the presence of magneto and thermal radiation effects
is studied. The fluid is assumed to be incompressible and dense. The nonlinear coupled parabolic partial differential equations
governing the flow are transformed into the non-similar boundary layer equations, which are then solved numerically using
the Keller box method. The effects of the mixed convection parameter R
i, the angle of inclination α, the magnetic parameter M and the radiation–conduction parameter R
d on the velocity and temperature profiles as well as on the local skin friction and local heat transfer parameters. For some
specific values of the governing parameters, the results are compared with those available in the literature and a fairly
good agreement is obtained. 相似文献
6.
The effects of viscous dissipation are considered for natural convection flow past a semi-infinite inclined plate with variable
surface temperature. Velocity and temperature profiles, skin friction, and rate of heat transfer are obtained. The effects
of Grashof and Prandtl numbers, inclination angle, exponent in the wall temperature variation law, and viscous dissipation
parameter on the flow are discussed. It is shown that the time required to reach steady states increases with increasing Prandtl
number of the fluid. In addition, an increase in the plate temperature due to viscous dissipation was found to lead to a rise
in the average skin friction and a decrease in the average Nusselt number. 相似文献
7.
The jet boiling heat transfer of a bar water–CuO particle suspensions (nanofluids) jet impingement on a large flat surface
was experimentally investigated. The experimental results were compared with those from water. The quantificational effects
of the nanoparticles concentration and the flow conditions on the nucleate boiling heat transfer and the critical heat flux
(CHF) were investigated. The experimental data showed that the jet boiling heat transfer for the water–CuO nanofluid is significantly
different from those for water. The nanofluids have poor nucleate boiling heat transfer compared with the base fluid due to
that a very thin nanoparticle sorption layer was formed on the heated surface. The CHF for the nanofluid increased compared
with that of water. The reasons were that the solid–liquid contact angle decreased due to a very thin sorption layer on the
heated surface and the jet and agitating effect of the nanoparticles on the subfilm layer enhance supply of liquid to the
surface. 相似文献
8.
This work presents a parametric study and optimization of a single impinging jet with cross flow to enhance heat transfer
with two design variables. The fluid flow and heat transfer have been analyzed using three-dimensional compressible Reynolds-averaged
Navier–Stokes equations with a uniform heat flux condition being applied to the impingement plate. The aspect ratio of the
elliptic jet hole and the angle of inclination of the jet nozzle are chosen as the two design variables, and the area-averaged
Nusselt number on a limited target plate is set as the objective function. The effects of the design variables on the heat
transfer performance have been evaluated, and the objective function has been found to be more sensitive to the angle of inclination
of the jet nozzle than to the aspect ratio of the elliptic jet hole. The optimization has been performed by using the radial
basis neural network model. Through the optimization, the area-averaged Nusselt number increased by 7.89% compared to that
under the reference geometry. 相似文献
9.
The present investigation, involving the simultaneous heat and mass transfer is concerned with a numerical study of transient natural convection flow past an impulsively started inclined plate. Crank-Nicolson implicit finite difference method is used to solve the unsteady, non-linear and coupled governing equations. In order to check the accuracy of the numerical results, the present study is compared with available exact solution and are found to be in good agreement. Numerical results are obtained for various parameters. The steady-state velocity, temperature and concentration profiles, local and average skin friction, local and average Nusselt number, local and average Sherwood number are shown graphically. It is observed that local wall shear stress decreases as an angle of inclination { decreases. 相似文献
10.
K. Das 《国际流体数值方法杂志》2012,70(1):96-113
The influence of partial slip, thermal radiation, chemical reaction and temperature‐dependent fluid properties on heat and mass transfer in hydro‐magnetic micropolar fluid flow over an inclined permeable plate with constant heat flux and non‐uniform heat source/sink is studied. The transverse magnetic field is assumed as a function of the distance from the origin. Also it is assumed that the fluid viscosity and the thermal conductivity vary as an inverse function and linear function of temperature, respectively. With the use of the similarity transformation, the governing system of non‐linear partial differential equations are transformed into non‐linear ordinary differential equations and are solved numerically using symbolic software MATHEMATICA 7.0 (Wolfram Research, Champaign, IL). The numerical values obtained for the velocity, microrotation, temperature, species concentration, skin friction coefficient and the Nusselt number are presented through graphs and tables for several sets of values of the parameters. The effects of various physical parameters on the flow and heat transfer characteristics are discussed.Copyright © 2011 John Wiley & Sons, Ltd. 相似文献
11.
The governing non-linear high-order, sixth-order in space and third-order in time, differential equation is constructed for the unsteady flow of an incompressible conducting fourth-grade fluid in a semi-infinite domain. The unsteady flow is induced by a periodically oscillating two-dimensional infinite porous plate with suction/blowing, located in a uniform magnetic field. It is shown that by augmenting additional boundary conditions at infinity based on asymptotic structures and transforming the semi-infinite physical space to a bounded computational domain by means of a coordinate transformation, it is possible to obtain numerical solutions of the non-linear magnetohydrodynamic equation. In particular, due to the unsymmetry of the boundary conditions, in numerical simulations non-central difference schemes are constructed and employed to approximate the emerging higher-order spatial derivatives. Effects of material parameters, uniform suction or blowing past the porous plate, exerted magnetic field and oscillation frequency of the plate on the time-dependent flow, especially on the boundary layer structure near the plate, are numerically analysed and discussed. The flow behaviour of the fourth-grade non-Newtonian fluid is also compared with those of the Newtonian fluid. 相似文献
12.
This paper presents the characteristics of flow behavior and thermal fields of both free and impingement jets issued from circular orifice nozzle at Re = 9,700. The flow behavior of a single round jet and impingement jet were observed by smoke flow visualization recorded by a high speed video camera with 5,000 frames per second. Heat transfer coefficient on the impingement surface was calculated varying the Reynolds number and the separation distance between nozzle exit and plate. Time-series analysis was applied to the visualization image to get the information of time variation of flow behavior. Probability distribution of vortex scale induced by the jet at discrete positions was investigated. Experimental results show that the potential core is not a continuous phenomenon with time and the frequency of vortex ring formation have similar features regardless of whether the impingement plate was set on or not, furthermore the time-series analysis with flow visualization images makes clear the detailed flow behavior. 相似文献
13.
An experimental study was performed to characterize the boiling heat transfer of impinging circular submerged jets on simulated microelectronic chips with a nominal area of 5 mm × 5 mm. The heat transfer modes included natural convection, partially developed nucleate boiling, fully developed nucleate boiling and critical heat flux. The study included the effects of jet parameters and fluid subcooling on the nucleate boiling. The results showed that the nucleate boiling data varied only with fluid subcooling regardless of jet parameters and that both the pool and impingement nucleate boiling curves at the same subcooling condition were well correlated. The high heat flux portions of the boiling curves with jet exit velocities greater than 10 m/s were corrected for the elevated saturation temperature. A new expression was developed with an interpolation method to construct the partially developed nucleate boiling curve. 相似文献
14.
An experimental investigation was carried out on the heat transfer due to a submerged slot jet of water impinging on a circular cylinder in crossflow. The cylinder diameter and the slot width are of the same order of magnitude, specifically Ds = 2.0 and 3.0 mm and Dc = 2.5 and 3.0 mm. The experimental apparatus allowed variation of the slot width, the cylinder diameter, and the distance from nozxle exit to heater. Conditions of impingement from the bottom (ascending flow) were taken into consideration as well as impingement from above (descending flow). The Nusselt number was determined as a function of Reynolds and Prandtl numbers in the range 1.5 × 103 < Re < 2.0 × 104, 2.7 < Pr < 7.0, and 1.5 ≤ z/Ds ≤ 10. The experimental data were correlated with a simple equation that fits 90% of the data with a precision of 20%. 相似文献
15.
Gh. Juncu 《Heat and Mass Transfer》2005,41(12):1095-1102
Numerical methods are used to investigate the transient, forced convection heat/mass transfer from a finite flat plate to a steady stream of viscous, incompressible fluid. The temperature/concentration inside the plate is considered uniform. The heat/mass balance equations were solved in elliptic cylindrical coordinates by a finite difference implicit ADI method. These solutions span the parameter ranges 10 Re 400 and 0.1 Pr 10. The computations were focused on the influence of the product (aspect ratio) × (volume heat capacity ratio/Henry number) on the heat/mass transfer rate. The occurrence on the plates surface of heat/mass wake phenomena was also studied. 相似文献
16.
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、 Re_{w} , Y/W 和 S/W 等
参数对 \sqrt {\overline{u^2}} / U_m 的影响比对 \sqrt {\overline{v^2}} / U_m 强,并且切
应力 \overline {uv} /U_m^2 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. 相似文献
17.
An experimental investigation is made to study the flow characteristics of slot jet impingement on a cylinder. The velocity profiles and pressure distribution around the cylinder are reported for various parameters namely, the flow rate, width of the nozzle, distance of the cylinder from the jet exit and eccentricity of the cylinder to the jet axis.
Nomenclature B breadth of the nozzle at the exit - D diameter of the cylinder - C p pressure coefficient - g acceleration due to gravity - L distance of the cylinder from jet exit - P a atmospheric pressure - P c static pressure along the jet center-line - P 0 stagnation pressure - P W wall static pressure - Re D Reynolds numberu j D/ a - Re W Reynolds numberu j W/ a - r distance measured from cylinder surface in radial direction - r m position of maximum velocity from cylinder surface - r 0.5 half width of the jet - u mean velocity - u j mean velocity at the jet exit - u m maximum velocity - W width of the nozzle - a density of air - m density of mercury - w density of water - absolute viscosity - kinematic viscosity 相似文献
Experimentelle Untersuchung über die Strömungseigenschaften eines Düsenstrahls, der auf einen Zylinder aufprallt
Zusammenfassung Es wurde eine experimentelle Untersuchung gemacht, um die Strömungseigenschaften eines Düsenstrahls zu unterschen, der auf einen Zylinder prallt. Die Geschwindigkeitsprofile und die Druckverteilungen an dem Zylinder wurden für unterschiedliche Parameter dokumentiert. Die Parameter sind die Strömungsgeschwindigkeit, Düsengröße, Abstand zwischen Zylinder und Strahlaustritt und die Exzentrizität von Zylinder und Strahlachse.
Nomenclature B breadth of the nozzle at the exit - D diameter of the cylinder - C p pressure coefficient - g acceleration due to gravity - L distance of the cylinder from jet exit - P a atmospheric pressure - P c static pressure along the jet center-line - P 0 stagnation pressure - P W wall static pressure - Re D Reynolds numberu j D/ a - Re W Reynolds numberu j W/ a - r distance measured from cylinder surface in radial direction - r m position of maximum velocity from cylinder surface - r 0.5 half width of the jet - u mean velocity - u j mean velocity at the jet exit - u m maximum velocity - W width of the nozzle - a density of air - m density of mercury - w density of water - absolute viscosity - kinematic viscosity 相似文献
18.
Transient natural convection boundary layer flow of an incompressible viscous fluid past an impulsively moving semi- infinite
vertical cylinder is considered. The temperature and concentration of the cylinder surface are taken to be uniform. The unsteady,
nonlinear and coupled governing equations of the flow are solved using an implicit finite difference scheme. The finite difference
scheme is unconditionally stable and accurate. Numerical results are presented with various sets of parameters for both air
and water. Transient effects of velocity, temperature and concentration profiles are analyzed. Local and average skin friction,
rates of heat and mass transfer are shown graphically.
Received on 1 November 1999 相似文献
19.
Local heat transfer from an impinging high temperature jet is studied using a method based on the heat thin foil technique and on the infrared thermography. Heat thin foil technique is used to impose several heat fluxes. For each flux, the temperature distribution is recorded using infrared imaging. Local heat transfer coefficients and adiabatic wall temperatures are determined by means of a linear regression method. This procedure is validated for a single round jet impinging on a flat plate for a range of injection temperatures. To cite this article: M. Fénot et al., C. R. Mecanique 333 (2005). 相似文献
20.
In this paper, we study the unsteady coupled heat and mass transfer of two-dimensional MHD fluid over a moving oscillatory stretching surface with Soret and Dufour effects. Viscous dissipation effects are adopted in the energy equation. A uniform magnetic field is applied vertically to the flow direction. The governing equations are reduced to non-linear coupled partial differential equations and solved by means of homotopy analysis method (HAM). The effects of some physical parameters such as magnetic parameter, Dufour number, Soret number, the Prandtl num- ber and the ratio of the oscillation frequency of the sheet to its stretching rate on the flow and heat transfer characteristics are illustrated and analyzed. 相似文献