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Effect of the Pattern of Initial Perturbations on the Steady Pipe Flow Regime

机译:初始扰动方式对稳态管道流态的影响

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摘要

The influence of the inlet flow formation mode on the steady flow regime in a circular pipe has been investigated experimentally. For a given inlet flow formation mode the Reynolds number Re{sup}* at which the transition from laminar to turbulent steady flow occurred was determined. With decrease in the Reynolds number the difference between the resistance coefficients for laminar and turbulent flows decreases. At a Reynolds number approximately equal to 1000 the resistance coefficients calculated from the Hagen-Poiseuille formula for laminar steady flow and from the Prandtl formula for turbulent steady flow are equal. Therefore, we may assume that at Re < 1000 steady pipe flow can only be laminar and in this case it is meaningless to speak of a transition from one steady pipe flow regime to the other. The previously published results [1-9] show that the Reynolds number at which laminar goes over into turbulent steady flow decreases with increase in the intensity of the inlet pulsations. However, at the highest inlet pulsation intensities realized experimentally, turbulent flow was observed only at Reynolds numbers higher than a certain value, which in different experiments varied over the range 1900-2320 [10]. In spite of this scatter, it has been assumed that in the experiments a so-called lower critical Reynolds number was determined, such that at higher Reynolds numbers turbulent flow can be observed and at lower Reynolds numbers for any inlet perturbations only steady laminar flow can be realized. In contrast to the lower critical Reynolds number, the Re{sup}* values obtained in the present study, were determined for given (not arbitrary) inlet flow formation modes. In this study, it is experimentally shown that the Re{sup}* values depend not only on the pipe inlet pulsation intensity but also on the pulsation flow pattern. This result suggests that in the previous experiments the Re{sup}* values were determined and that their scatter is related with the different pulsation flow patterns at the pipe inlet. The experimental data so far obtained are insufficient either to determine the lower critical Reynolds number or even to assert that this number exists for a pipe at all.
机译:实验研究了入口流形成方式对圆形管内稳态流态的影响。对于给定的入口流形成模式,确定了发生从层流到湍流稳定流的转变的雷诺数Re {sup} *。随着雷诺数的减少,层流和湍流阻力系数之间的差异减小。在雷诺数大约等于1000时,根据Hagen-Poiseuille公式计算的层流稳定流和根据Prandtl公式计算的湍流稳定流的阻力系数相等。因此,我们可以假设在Re <1000时,稳态管道流量只能是层流状态,在这种情况下,谈论从一种稳态管道流量状态过渡到另一种稳态管道流量是没有意义的。先前发表的结果[1-9]表明,层流进入湍流稳定流的雷诺数随入口脉动强度的增加而减小。然而,在实验中实现的最高进气脉动强度下,仅在雷诺数高于一定值时才观察到湍流,在不同的实验中,雷诺数在1900-2320范围内变化[10]。尽管存在这种分散性,但是已经假设在实验中确定了所谓的较低的临界雷诺数,使得在较高的雷诺数下,可以观察到湍流,而对于较低的雷诺数,对于任何入口扰动,只能观察到稳定的层流被实现。与较低的临界雷诺数相反,本研究中获得的Re {sup} *值是针对给定的(不是任意的)入口流形成模式确定的。在这项研究中,实验表明Re {sup} *值不仅取决于管道入口的脉动强度,而且还取决于脉动流型。该结果表明,在先前的实验中,确定了Re {sup} *值,并且它们的散布与管道入口处的不同脉动流模式有关。迄今为止获得的实验数据不足以确定较低的临界雷诺数,甚至不足以断言该数字对于管道完全存在。

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