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Tsing Ma bridge deck under skew winds - part I : aerodynamic coefficients

机译:斜风下的青马大桥桥面-第一部分:空气动力系数

摘要

This paper aims to measure six static aerodynamic coefficients, while a companion paper addresses the measurement of eight flutter derivatives, of a typical oblique strip of the Tsing Ma suspension bridge deck under skew winds. The wind tunnel test technique developed for the aerodynamic coefficient measurement includes the design of oblique sectional models, the development of a test rig and a measurement system, and the analysis of test results. The effects of model end angle on the aerodynamic coefficients are investigated and found to be very small on lift, drag and pitching moment coefficients. The measured results are then fitted to obtain the six aerodynamic coefficient curves as functions of both wind inclination and yaw angle, which will be used in a later comparison of buffeting response of the bridge between field measurement and analysis. The measurement results reveal that the drag, lift and pitching moment coefficients are much larger than the crosswind force, rolling moment and yawing moment coefficients. The variation of lift coefficient with wind yaw angle is small, but the value of drag coefficient decreases with increasing wind yaw angle and the value of pitching moment coefficient increases with increasing wind yaw angle. The obtained six aerodynamic coefficient curves are also used to examine the currently used cosine rule for buffeting analysis of a bridge under yaw winds. It is found that the traditional cosine rule is generally inadequate, particularly in the cases of large wind yaw angle.
机译:本文旨在测量六种静态空气动力系数,而另一篇论文则涉及在偏风作用下对青马悬索桥甲板的典型倾斜带的八个颤振导数的测量。为测量空气动力系数而开发的风洞测试技术包括斜截面模型的设计,测试设备和测量系统的开发以及测试结果的分析。研究了模型端角对空气动力学系数的影响,发现对升力,阻力和俯仰力矩系数影响很小。然后对测量结果进行拟合,以得到作为风倾角和偏航角函数的六个空气动力学系数曲线,这些曲线将在以后的实地测量和分析之间的桥梁抖振响应比较中使用。测量结果表明,阻力,升力和俯仰力矩系数远大于侧风力,侧倾力矩和偏航力矩系数。升力系数随风偏角的变化很小,但阻力系数的值随风偏角的增加而减小,俯仰力矩系数的值随风偏角的增加而增加。所获得的六个空气动力学系数曲线还用于检查当前使用的余弦法则,用于偏航风作用下桥梁的抖振分析。发现传统的余弦法则通常是不合适的,特别是在大的偏航角情况下。

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