Bubbly turbulent Taylor-Couette (TC) flow is globally and locally studied atReynolds numbers of Re = 5 x 10^5 to 2 x 10^6 with a stationary outer cylinderand a mean bubble diameter around 1 mm. We measure the drag reduction (DR)based on the global dimensional torque as a function of the global gas volumefraction a_global over the range 0% to 4%. We observe a moderate DR of up to 7%for Re = 5.1 x 10^5. Significantly stronger DR is achieved for Re = 1.0 x 10^6and 2.0 x 10^6 with, remarkably, more than 40% of DR at Re = 2.0 x 10^6 anda_global = 4%. To shed light on the two apparently different regimes of moderate DR andstrong DR, we investigate the local liquid flow velocity and the local bubblestatistics, in particular the radial gas concentration profiles and the bubblesize distribution, for the two different cases; Re = 5.1 x 10^5 in the moderateDR regime and Re = 1.0 x 10^6 in the strong DR regime, both at a_global = 3 +/-0.5%. By defining and measuring a local bubble Weber number (We) in the TC gapclose to the IC wall, we observe that the crossover from the moderate to thestrong DR regime occurs roughly at the crossover of We ~ 1. In the strong DRregime at Re = 1.0 x 10^6 we find We > 1, reaching a value of 9 (+7, -2) whenapproaching the inner wall, indicating that the bubbles increasingly deform asthey draw near the inner wall. In the moderate DR regime at Re = 5.1 x 10^5 wefind We ~ 1, indicating more rigid bubbles, even though the mean bubblediameter is larger, namely 1.2 (+0.7, -0.1) mm, as compared to the Re = 1.0 x10^6 case, where it is 0.9 (+0.6, -0.1) mm. We conclude that bubbledeformability is a relevant mechanism behind the observed strong DR. Theselocal results match and extend the conclusions from the global flow experimentsas found by van den Berg et al. (2005) and from the numerical simulations byLu, Fernandez & Tryggvason (2005).
展开▼
机译:气泡和湍流泰勒-库埃特(TC)流是全球性的和局部性的研究,雷诺数Re = 5 x 10 ^ 5至2 x 10 ^ 6,外筒固定,平均气泡直径约为1 mm。我们在0%至4%的范围内,根据整体尺寸扭矩作为整体气体体积分数a_global的函数来测量减阻(DR)。对于Re = 5.1 x 10 ^ 5,我们观察到高达7%的中等DR。当Re = 1.0 x 10 ^ 6和2.0 x 10 ^ 6时,DR显着增强,在Re = 2.0 x 10 ^ 6且a_global = 4%时,DR显着超过40%。为了阐明中度DR和强DR的两种明显不同的状态,我们研究了两种情况下的局部液体流速和局部气泡统计量,尤其是径向气体浓度分布和气泡大小分布。在a_global = 3 +/- 0.5%时,在中度DR方案中Re = 5.1 x 10 ^ 5,在强DR方案中Re = 1.0 x 10 ^ 6。通过定义和测量靠近IC壁的TC间隙中的局部气泡韦伯数(We),我们观察到从中度DR到强DR态的交叉大约发生在We〜1的交叉处。 1.0 x 10 ^ 6我们发现We> 1,接近内壁时达到9(+7,-2)的值,这表明气泡在靠近内壁时逐渐变形。在Re = 5.1 x 10 ^ 5的中等DR态下,我们将We〜1表示为更大的气泡,即使平均气泡直径比Re = 1.0 x10大,也就是1.2(+0.7,-0.1)mm ^ 6的情况,为0.9(+0.6,-0.1)毫米。我们得出结论,气泡变形能力是观察到的强DR背后的相关机制。这些局部结果与van den Berg等人发现的整体流动实验相吻合并扩展了结论。 (2005年)以及Lu,Fernandez和Tryggvason(2005年)的数值模拟。
展开▼