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Investigation of the upstream conditions and surface roughness in turbulent boundary layer.

机译:湍流边界层上游条件和表面粗糙度的研究。

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In this investigation, the incompressible zero-pressure-gradient turbulent boundary layers are investigated in light of the effect of the Reynolds number, the upstream conditions, and roughness. The experiments at very high Reynolds number were performed using cross hot-wire technique at the University of Western Ontario (UWO) on both a smooth surface and a rough surface. The range of the Reynolds number based on the momentum thickness was achieved from 30,000 up to 120,000. Wind tunnel speeds of 10 m/s and 20 m/s were set up in order to investigate the effect of the upstream conditions, the local Reynolds number effect and roughness effect on the downstream flow. Also, the experimental data from various researchers was collected and analyzed in order to study the effect of the Reynolds number, the upstream conditions, and the roughness in outer flow and inner flow.; Here, the scalings of George and Castillo (1997) for the mean velocity profiles and the Reynolds stress are used for analysis and compared with the results of the classical scalings determined by the log-law. It is shown that the mean deficit profiles in outer scaling are affected by the upstream conditions and they collapse in one curve for a given set of the upstream conditions even at very high Reynolds number. This result is contrary to the common belief about the true asymptotic state. Furthermore, the shape of the curve depends on the upstream conditions. On the other hand, it is shown that there is no apparent upstream condition effect in inner flow. Moreover, the true asymptotic profile (self-preserving) solution for the outer flow is found when the profiles are normalized by the Zagarola/Smits (1998) scaling, Uδ*/δ. This scaling successfully remove all the effects of the Reynolds number, the upstream conditions, and the roughness.; The Reynolds stress profiles are investigated in order to search the effect of the Reynolds number and the upstream conditions and it is found that the cross wise component of normal stress, υ2 > /U, in the outer variables is affected mostly by the upstream conditions among other Reynolds stress components. For fixed upstream conditions the cross wise component of the Reynolds stress tend to collapse in one curve. However, the Reynolds stresses profiles in the inner variables are shown to be dependent on the Reynolds number not the upstream conditions.; More importantly, the analytical form of the skin-friction law for rough surface turbulent boundary layer, which is also applicable for smooth surface, is found as a function of the local Reynolds number, δ+, and the roughness parameter, κ+. Furthermore, the boundary layer parameters and the growth rate of the boundary layer can be represented in analytical form as functions of δ+ and κ +. This results were induced using the composite velocity profiles for rough surface and Near-Asmyptotics method of George and Castillo (1997). The predictability of the skin-friction and the boundary layer parameters will provide great tools for the practical engineering design and turbulence modeling.
机译:在这项研究中,根据雷诺数,上游条件和粗糙度的影响,研究了不可压缩的零压力梯度湍流边界层。雷诺数很高的实验是在西安大略大学(UWO)使用交叉热线技术在光滑表面和粗糙表面上进行的。基于动量厚度的雷诺数范围达到了30,000到120,000。为了研究上游条件,局部雷诺数效应和粗糙度效应对上游条件的影响,设置风洞速度分别为10 m / s 和20 m / s 。下游流量。此外,为了研究雷诺数,上游条件以及外流和内流粗糙度的影响,收集并分析了来自各个研究人员的实验数据。在这里,George和Castillo(1997)对平均速度剖面和雷诺应力的标度用于分析,并与由对数定律确定的经典标度的结果进行比较。结果表明,外部结垢的平均缺陷分布受上游条件的影响,即使在非常高的雷诺数下,对于给定的一组上游条件,它们也以一条曲线塌陷。该结果与关于真实渐近状态的普遍看法相反。此外,曲线的形状取决于上游条件。另一方面,表明内部流动中没有明显的上游条件效应。此外,当通过Zagarola / Smits(1998)缩放比例, U δ归一化归一化轮廓时,可以找到外流的真正渐近轮廓(自保)解。 * /δ。这种缩放成功地消除了雷诺数,上游条件和粗糙度的所有影响。为了研究雷诺数和上游条件的影响,研究了雷诺应力分布图,发现正应力的横向分量<&upsi; 2 U ,在外部变量中,主要受上游条件以及其他雷诺应力分量的影响。对于固定的上游条件,雷诺应力的横向分量趋向于沿一条曲线塌陷。但是,内部变量中的雷诺应力分布显示为取决于雷诺数而不是上游条件。更重要的是,发现粗糙表面湍流边界层的皮肤摩擦定律的解析形式(也适用于光滑表面)是局部雷诺数,δ + 和粗糙度参数κ + 。此外,边界层参数和边界层的生长速率可以解析形式表示为δ + 和κ + 的函数。这个结果是由乔治和卡斯蒂略(George and Castillo,1997)使用粗糙表面的复合速度剖面和近渐近线法得出的。蒙皮摩擦和边界层参数的可预测性将为实际工程设计和湍流建模提供很好的工具。

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