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Laminar Flow and Pressure Loss of Power-Law Fluids in Pipes with an Axisymmetric Sudden Contraction

机译:管道中电力法流体的层流,轴对称突然收缩

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摘要

A steady laminar flow of an incompressible non-Newtonian fluid (inelastic power-law fluid; n<1) in pipelines with an axisymmetric sudden contraction was studied by experiments on pressure drops and a theoretical analysis using the finite difference methods. The main results obtained are as follows:(1) The sudden contraction loss decreases with increase in Reynolds number. The effects of the power-law index and the diameter ratio are small in the laminar flow and within experimental error in the range of the present experiments.(2) The present numerical method based on Kawamura's finite difference scheme and curvilinear grid points developed by Thompson et al. is useful for the contraction pipe flow in the range of 102-103 of Reynolds number.(3) The pressure at pipe wall has a minimum right after the sudden contraction section and through the recovery process, it becomes to decrease monotonously. In this monotonous region, the pressure under the same Reynolds number increases with decrease of the power-law index.(4) The pressure at pipe axis varies approximately as the pressure at pipe wall does. As Reynolds number becomes sufficiently small, the minimum right after the sudden contraction section disappears.(5) The velocity profile does not have a monotonous shape in the corner region of upstream side and in the separation region of downstream, and the maximum velocity at non-axial position appears in the downstream side of contraction pipe.(6) The vortex region in the corner of upstream side becomes larger with increase in Reynolds number. As Reynolds number becomes sufficiently large, the separation vortex region appears in the downstream side.
机译:通过使用有限差分方法的压降和理论分析,研究了不可压缩的非牛顿流体(无弹性动力 - 法流体; N <1)的稳定层流量。使用有限差分方法,研究了轴对称突然收缩的管道中。所获得的主要结果如下:(1)突然收缩损失随着雷诺数的增加而降低。电力法指数的效果和直径比在层流中较小,在本实验的范围内的实验误差中。(2)基于Kawamura有限差分方案和由Thompson开发的曲线网格点的现有数值方法等等。对于雷诺数102-103的收缩管流量是有用的。(3)管壁的压力在突然收缩部分和通过回收过程之后的最小右,它变得单调减少。在这种单调的区域中,相同雷诺数下的压力随着电力法指数的减少而增加。(4)管道轴的压力大致随管壁的压力而变化。由于雷诺数变得足够小,突然收缩部分之后的最小右侧。(5)速度曲线在上游侧的角落区域和下游的分离区域中没有单调形状,并且在非下游的最大速度 - 轴向轴的轴向位置出现在收缩管的下游侧。(6)上游侧角落的涡旋区域随着雷诺数的增加而变大。由于雷诺数变得足够大,分离涡旋区域出现在下游侧。

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