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COMPUTATION OF VELOCITY PROFILES AND PRESSURE COEFFICIENTS FOR A LAMINAR FLOW OF AIR OVER STAGGERED ARRAY OF TUBES

机译:空气中空气流动的速度分布和压力系数的计算

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In this study a two dimensional, steady state and incompressible laminar flow for staggered tube arrays in crossflow is investigated numerically. A finite-volume method is used to discretize and solve the governing Navier-Stokes equations for the geometries expressed by a boundary-fitted coordinate system. Solutions for Reynolds numbers of 100, 300, and 500 are obtained for a tube bundle with 10 longitudinal rows. Local velocity profiles on top of each tube and corresponding pressure coefficient are presented at nominal pitch-to-diameter ratios of 1.33, 1.60, and 2.00 for ES, ET, and RS arrangements. Differences in location of separation points are compared for three different arrangements. The predicted results on flow field for pressure coefficient showed a good agreement with available experimental measurements.
机译:在该研究中,在数值上研究了用于交叉流量的交错管阵列的二维,稳态和不可压缩的层流。有限体积法用于离散和解决管理由边界坐标系表示的几何形状的管理Navier-Stokes方程。为具有10个纵向行的管束获得100,300和500的雷诺数的解决方案。每个管子顶部和相应的压力系数的局部速度曲线以ES,ET和RS布置的标称间距比率为1.33,1.60和2.00。比较分离点位置的差异,以3个不同的布置。压力系数流场的预测结果显示出具有可用实验测量的良好一致性。

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