Turbulence Structure in the Leading-Edge Separation Zone of a Blunt Circular Cylinder

M. Kiya, Toshiya Nozawa
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引用次数: 8

Abstract

This paper describes experimentally the turbulence structure in the separation zone at the leading edge of a blunt circular cylinder aligned with a uniform main flow. The experiment was made in a wind tunnel at a Reynolds number of 200 000. Turbulent velocities were measured by split-film probes and surface-pressure fluctuations by semiconductor strain-gauged pressure transducers mounted inside the cylinder. Profiles of the time-mean and r. m. s. values of the fluctuating quantities and the Reynolds shearing stress in the separation zone are presented. Cross correlations and power spectra of the surface pressures yield the translation velocity of large-scale vortices and the frequency at which they are shed from the separation zone. The unsteady nature of the flow is demonstrated by the reverse-flow intermittency and by the frequency of switching of the local-flow direction. Moreover, the above properties are discussed in comparison with those of a leading-edge separation zone of a two-dimensional blunt plate.
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钝圆柱前缘分离区的湍流结构
本文实验描述了均匀主流对准钝圆柱前缘分离区的湍流结构。实验在雷诺数为20万的风洞中进行。湍流速度由裂膜探头测量,表面压力波动由安装在气缸内的半导体应变式压力传感器测量。给出了分离区内波动量和雷诺数剪切应力的时间平均值和r.m.s.曲线。表面压力的相互关系和功率谱可得出大尺度涡旋的平移速度和它们从分离带脱落的频率。紊流的非定常性主要表现在紊流的逆流动间断性和局部流动方向切换的频率上。并与二维钝板前缘分离带的特性进行了比较。
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