...
首页> 外文期刊>Journal of Fluid Mechanics >Saltation and incipient suspension above a flat particle bed below a turbulent boundary layer
【24h】

Saltation and incipient suspension above a flat particle bed below a turbulent boundary layer

机译:湍流边界层下方平坦颗粒层上方的盐析和初始悬浮

获取原文
获取原文并翻译 | 示例
           

摘要

Experiments were conducted in a wind tunnel in which a turbulent boundary layer was naturally grown over flat beds of three types of nearly mono-disperse spherical particles with different diameters, densities and coefficient of restitution (r) (snow, 0.48 mm, 910 kg m(-3); mustard seeds, 1.82 mm, 1670 kg m(-3), r = 0.7; ice particles, 2.80 mm, 910 kg m(-3), r = 0.8-0.9). The surface wind speeds (defined by the friction velocity u*) were varied between 1.0 and 1.9 times the threshold surface wind speed (defined by u*(t)). The trajectories, and ejection and impact velocities of the particles were recorded and analysed, even those that were raised only about one diameter into the flow. Measurements of the average horizontal flux of saltating particles per unit area, f(z), at each level z above the surface showed that, for u*/u*t less than or equal to 1.5, f(z) is approximately independent of the particle density and decreases exponentially over a vertical scale length l(f), that is about 3 to 4 times the estimated mean height of the particle trajectories < h >. Numerical simulations of saltating grains were computed using the measured probabilities of ejection velocities and the mean velocity profile of the air flow, but neglecting the direct effect of the turbulence. The calculated mean values of the impact velocities and the trajectory dimensions were found to agree with the measurements in the saltation range, where u*/u*(t) < 1.5. Similarly, in this range the simulations of the horizontal flux profile and integral are also consistent with the measurements and with Bagi old's u*(3) formula, respectively. When u*/u*(t) greater than or equal to 1.5, and u*/ V-T greater than or equal to 1/10, where V-T is the settling velocity, a transition from saltation to suspension occurs. This is indicated by the change in the mean mass flux profile which effectively becomes uniform with height (z) up to the top of the boundary layer. An explanation is provided for this low value of turbulence at transition relative to the settling velocity in terms of the random motion of the particles under the action of the turbulence when they reach the tops of their parabolic trajectories. The experiments show that, as u*/u*(t) increases from 1.0 to 1.9 the normalized mean vertical impact velocity < V-31>/u* decreases by nearly 60% to about 0.6, which is less than 50% of the value for fluid particles. There is also a decrease in the vertical and horizontal component of the ejection velocity to values of 0.8 and 2.3, which are much less than their values in the saltation regime. We hypothesize that at the transition from saltation to suspension the ejection process changes quite sharply from being determined by impact collisions to being the result of aerodynamic lift forces and upward eddy motions. [References: 40]
机译:实验是在风洞中进行的,在该风洞中,湍流边界层自然生长在具有不同直径,密度和恢复系数(r)(雪,0.48 mm,910 kg m (-3);芥菜籽,1.82毫米,1670千克米(-3),r = 0.7;冰粒,2.80毫米,910千克米(-3),r = 0.8-0.9)。表面风速(由摩擦速度u *定义)在阈值表面风速(由u *(t)定义)的1.0到1.9倍之间变化。记录并分析颗粒的轨迹,喷射速度和冲击速度,甚至是那些仅上升到流中约一个直径的颗粒。在表面上方每个水平z处,每单位面积的盐化颗粒平均水平通量f(z)的测量结果表明,对于u * / u * t小于或等于1.5,f(z)近似独立于粒子密度在垂直尺度长度l(f)上呈指数下降,约为粒子轨迹的估计平均高度的3-4倍。使用测得的喷射速度和气流的平均速度分布来计算盐化颗粒的数值模拟,但忽略了湍流的直接影响。发现冲击速度和轨迹尺寸的计算平均值与盐化范围内的测量值一致,其中u * / u *(t)<1.5。同样,在此范围内,水平通量剖面和积分的模拟也分别与测量结果和Bagi old的u *(3)公式一致。当u * / u *(t)大于或等于1.5,并且u * / V-T大于或等于1/10时(其中V-T为沉降速度),会发生从盐析到悬浮的转变。这由平均质量通量分布图的变化表示,该变化有效地随着高度(z)直到边界层的顶部变得均匀。根据当颗粒到达其抛物线轨迹的顶部时在湍流作用下的颗粒的随机运动,相对于沉降速度的这种低湍流值提供了解释。实验表明,随着u * / u *(t)从1.0增加到1.9,归一化平均垂直冲击速度 / u *降低了近60%,降至约0.6,这不到其的50%。流体粒子的值。喷射速度的垂直和水平分量也减小到0.8和2.3的值,这远小于在盐析过程中的值。我们假设在从盐化到悬浮的过渡过程中,喷射过程的变化非常明显,从冲击碰撞确定到气动升力和向上涡流运动的结果。 [参考:40]

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号