首页> 外文会议>HTD-vol.375-3; American Society of Mechanical Engineers(ASME) International Mechanical Engineering Congress and Exposition vol.3; 20041113-19; Anaheim,CA(US) >EFFECT OF WALL THERMAL BOUNDARY CONDITIONS ON THE DEVELOPMENT OF THREE-DIMENSIONAL, UNSTEADY NATURAL CONVECTIVE FLOW IN A HORIZONTAL ENCLOSURE WITH A HEATED STRIP ON THE LOWER SURFACE
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EFFECT OF WALL THERMAL BOUNDARY CONDITIONS ON THE DEVELOPMENT OF THREE-DIMENSIONAL, UNSTEADY NATURAL CONVECTIVE FLOW IN A HORIZONTAL ENCLOSURE WITH A HEATED STRIP ON THE LOWER SURFACE

机译:壁面水平带加热带的水平热边界条件下壁热边界条件对三维非定常自然对流流动的影响

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Plow in a rectangular enclosure with a square vertical cross-section normal to the longitudinal coordinate direction and having a strip on the lower horizontal surface which is heated to a uniform high temperature has been numerically studied. Two wall thermal boundary conditions have been considered. In one, the longitudinal vertical side walls are cooled to a uniform low temperature and the horizontal top surface is adiabatic while in the other the longitudinal vertical side walls and the horizontal top surface are cooled to a uniform low temperature. In both cases, the square vertical end walls of the enclosure are adiabatic. It has been assumed that the flow is laminar and that the fluid properties are constant except for the density change with temperature which gives rise to the buoyancy forces. The unsteady, three-dimensional governing equations, expressed in dimension-less form, have been solved using a finite-difference procedure. The solution was started with no flow in the enclosure. The solution, in general, has the following parameters: the Rayleigh Number, Ha, the Prandtl number, Pr, the dimensionless longitudinal length of the enclosure relative to the size of the square cross-section, A_y, the dimensionless width of the heated strip on the lower surface relative to the size of the square cross-sectiqp, w_H, and the thermal boundary condition on the upper surface. Results have only been obtained for a Prandtl number of 0.7 and only results for w_H = 1/3 will be presented. Results have been obtained for values of A_y between 0.5 and 2 for Rayleigh numbers up to 5 x 10~5. In all cases, three-dimensional unsteady flow has been found to exist at the higher Rayleigh numbers. The conditions under which this unsteady flow develops and the effect of A_y on the variation of the mean Nusselt number with Rayleigh number and the effect of the wall surface boundary condition on these results has been investigated.
机译:数值研究了在矩形外壳中的犁,该犁具有垂直于纵向坐标方向的垂直截面为正方形且在下水平面具有加热到均匀高温的条形。已经考虑了两个壁热边界条件。在一个中,纵向竖直侧壁被冷却至均匀的低温,并且水平顶表面是绝热的,而在另一种情况中,纵向竖直侧壁和水平顶面被冷却至均匀的低温。在这两种情况下,外壳的方形垂直端壁都是绝热的。假定流动是层流的,并且流体的特性是恒定的,除了密度随温度的变化会引起浮力。使用有限差分法求解了以无量纲形式表示的非定常三维控制方程。解决方案开始时,机箱中没有任何流动。通常,该解决方案具有以下参数:瑞利数Ha,普朗特数Pr,相对于方形横截面尺寸的外壳的无量纲纵向长度A_y,加热带材的无量纲宽度相对于正方形十字截面的尺寸w_H和下表面的热边界条件。仅在0.7的Prandtl数下获得结果,并且仅显示w_H = 1/3的结果。对于高达5 x 10〜5的瑞利数,已经获得了A_y值介于0.5和2之间的结果。在所有情况下,都发现在较高的瑞利数下存在三维非定常流动。研究了这种不稳定流动的条件,以及A_y对平均Nusselt数随Rayleigh数变化的影响以及壁面边界条件对这些结果的影响。

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