Lift Coefficient Variation on a Cylinder Forced to Oscillate

J. Bernhardt, Jadran A. Mihailovic, C. F. Jines, Aziz Abouel-Fotouh, T. Corke, David R. Williams
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引用次数: 0

Abstract

The instantaneous pressure distribution around the azimuth of a cylinder undergoing forced oscillations is measured using an array of 18 miniature microphones. The microphones were placed at the midspan of the cylinder with 20 degree increments between each sensor. The Reynolds number for the experiments was 13,800. The cylinder is driven in a sinusoidal motion by a printed circuit motor with an amplitude A/D = 0.18 and with bare winding numbers (Ω = f/fn) of 0 ≤ Ω ≤ 1.1. Regions of lock-in between the cylinder motion and the lift coefficient were observed at dressed winding numbers of ω = 2:3, 1:2 and 1:1. Phase diagrams show two distinctly different synchronization mechanisms, one fundamental and the other a subharmonic type, which supports the findings of Ongoren and Rockwell (1988).
被迫振荡的圆柱体的升力系数变化
用18个微型传声器阵列测量了圆柱体在受强迫振荡时的方位周围的瞬时压力分布。麦克风被放置在圆柱体的中间,每个传感器之间有20度的增量。实验的雷诺数是13800。气缸由印刷电路电机驱动,其幅值a /D = 0.18,裸绕组数(Ω = f/fn)为0≤Ω≤1.1。在ω = 2:3, 1:2和1:1的修整绕组数下,观察到圆柱运动与升力系数之间的锁定区域。相位图显示了两种截然不同的同步机制,一种是基本同步机制,另一种是次谐波同步机制,这支持了Ongoren和Rockwell(1988)的发现。
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