Methods for determining the drag coefficient at gas injection from the surface of spherical particle

IF 0.3 Q4 MECHANICS
V. Arkhipov, S. Basalaev, Ksenia G. Perfllieva, S. Polenchuk, A. Usanina
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Abstract

New methods for studying the effect of gas injection from the surface of a solid spherical particle on its drag coefficient in the transient and self-similar regimes of flow around the particle have been presented. An advantage of the proposed methods is the ability to isolate in a pure form the effect of the mass flux from the particle surface (without the effect of other factors, for example, particle acceleration) on the drag coefficient. New results of an experimental study of the effect of air flow blowing on the drag coefficient of a solid perforated sphere in the Reynolds number range Re = 133÷9900 have been presented. It has been shown that the drag coefficient decreases when air is blown from the particle surface. As the Reynolds number Re increases, the drag coefficient CD upon gas injection in the transient flow regime decreases to a certain critical value corresponding to the onset of the self-similar regime. At the onset of the selfsimilar regime (reaching the critical value of CD), the drag coefficient increases with an increase in the Reynolds number and asymptotically tends to a constant value CD = 0.44. However, the opposite effect has been found for a small diameter of the particle (D = 1 cm) at a blowing velocity ue ≥ 1.3 m/s: an increase in the drag coefficient of the particle CD at air efflux from the particle surface in comparison with the drag coefficient value in the absence of gas flow injection (ue = 0 m/s). This is apparently associated with a change in the characteristics of the boundary layer of the particle due to the rearrangement of the flow profile near the spherical particle surface caused by a decrease in its size. An empirical dependence of the drag coefficient of a solid sphere on the ratio of the velocity of injection from the surface of the particle to the velocity of blowing CD = 0.15 + (0.44 - 0.15)/ (1 + 9ū/53.8) (with the coefficient of determination R2 = 0.89) has been obtained for a self-similar particle regime flow. Contribution of the authors: the authors contributed equally to this article. The authors declare no conflicts of interests.
球形颗粒表面注气阻力系数的测定方法
本文提出了一种研究固体球形颗粒表面气体注入对其瞬态和自相似流场阻力系数影响的新方法。所提出的方法的一个优点是能够以纯粹的形式分离来自粒子表面的质量通量对阻力系数的影响(没有其他因素,例如粒子加速度的影响)。本文给出了在雷诺数Re = 133÷9900范围内气流吹动对固体多孔球阻力系数影响的实验研究的新结果。结果表明,当空气从颗粒表面吹出时,阻力系数减小。随着雷诺数Re的增大,瞬态流型注气阻力系数CD减小到某一临界值,该临界值对应于自相似流型的开始。在自相似状态开始时(达到CD临界值),阻力系数随雷诺数的增加而增加,并渐近趋于恒定值CD = 0.44。然而,对于直径较小的颗粒(D = 1 cm),在吹速ue≥1.3 m/s时,则发现了相反的效果:与没有气流注入(ue = 0 m/s)时相比,颗粒表面气流流出时的阻力系数CD增加了。这显然与颗粒边界层特性的变化有关,这是由于球形颗粒表面附近流动剖面的重新排列引起的,这是由于颗粒尺寸减小引起的。对于自相似颗粒流,得到了实心球阻力系数与颗粒表面喷射速度与吹速之比的经验依赖关系:CD = 0.15 +(0.44 - 0.15)/(1 + 9′/53.8)(决定系数R2 = 0.89)。作者的贡献:作者对本文的贡献是平等的。作者声明没有利益冲突。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
0.90
自引率
66.70%
发文量
0
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