涡发生器对平板边界层影响的实验研究

عباس فاضل محمود
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摘要

本文对涡发生器VG的几何特性对边界层厚度(∂)和平板阻力系数(CD)的影响进行了实验研究。涡旋发生器在中高迎角时工作有效,因为它们“隐藏”在边界层下,在低角度时几乎无效。相对于边界层厚度的边界层高度使我们能够研究边界层延迟边界层分离的效果。如果考虑到两对VGs之间的干涉,两个VGs之间的距离也会对边界层产生影响。本文研究了三角涡发生器(h-涡发生器高度,d-两个涡发生器之间的平均距离)变化对平板边界层厚度和阻力系数的影响。为了确定最佳边界层厚度和阻力系数的变化,改变了涡发生器的测量方法。在平均自由流速度(U∞)为28 m/s的条件下进行了实验。实验是在乌克兰基辅UTAD-2大学(NAU)的风洞中进行的。
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AN EXPERIMENTAL STUDY OF THE EFFECT OF VORTEX GENERATOR ON THE FLAT-PLATE BOUNDARY LAYER
This paper is dealing with an experimental study to show the influence of the geometric characteristics of the vortex generators VG son the thickness of the boundary layer (∂) and drag coefficients (CD) of the flat plate. Vortex generators work effectively on medium and high angles of attack, since they are "hidden" under the boundary layer and practically ineffective at low angles. The height of VGs relative to the thickness of the boundary layer enables us to study the efficacy of VGs in delaying boundary layer separation. The distance between two VGs also has an effect on the boundary layer if we take into account the interference between two pairs of VGs. The effect of the changing in (h- the height of vortex generator, d- the average distance between tow vortex generators) on the thickness of the flat plate boundary layer and the drag coefficients has been studied for triangular vortex generator. The measurements of the vortex generator have been changed to determine the optimum boundary layer thickness and the change in drag coefficients. An experiment was done at an average free stream velocity, (U∞,) of 28 m/s. The experiment was conducted in the wind tunnel UTAD-2 University (NAU) Kiev, Ukraine.
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