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Experimental data on transport coefficients for developing laminar flow in isosceles triangular ducts using the naphthalene sublimation technique

机译:萘升华技术在等腰三角管中形成层流的输运系数实验数据

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摘要

The data presented in this article are related to the research article entitled "Transport coefficients for developing laminar flow in isosceles triangular ducts" (Parise and Saboya, 1999) [1]. The article describes an experiment involving the determination of transport coefficients in the laminar entrance region of 30°, 45°, 60° and 90° isosceles triangular ducts. Data were obtained by application of the naphthalene sublimation technique in conjunction with the heat to mass transfer analogy. Experimental conditions (duct sides made of naphthalene and base made of metal) simulated developing velocity and temperature fields in an isosceles triangular duct with isothermal lateral walls and adiabatic base. The Reynolds number ranged from 100 to 1800 and the duct length to hydraulic diameter ratio, from 2 to 40. The experiment consisted of mounting a test section (triangular duct) with the lateral walls made of naphthalene. Air was forced past the test section and naphthalene walls were weighed prior and after each data run, providing the rate of mass transfer for given flow conditions. Raw data, for a total of 77 experimental runs, include: test section geometry, air flow and mass transfer conditions. Processed data comprise the relevant non-dimensional groups, namely: Reynolds, non-dimensional axial duct length and Sherwood numbers.
机译:本文提供的数据与题为“在等腰三角管中形成层流的传输系数”的研究文章有关(Parise和Saboya,1999)[1]。该文章描述了一个实验,该实验涉及确定30°,45°,60°和90°等腰三角形管道的层流入口区域中的传输系数。通过应用萘升华技术结合热质传递类比获得数据。实验条件(由萘制成的导管侧面和由金属制成的底座)模拟了具有等温侧壁和绝热底座的等腰三角形导管中的发展速度和温度场。雷诺数在100到1800之间,管道长度与水力直径的比率在2到40之间。该实验包括安装一个带有萘侧壁的测试部分(三角形管道)。在每次数据运行之前和之后,将空气强行经过测试段,并称重萘壁,以提供给定流动条件下的传质速率。总共77个实验运行的原始数据包括:测试部分的几何形状,气流和传质条件。处理的数据包括相关的无量纲组,即:雷诺数,无量纲的轴向风管长度和舍伍德数。

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