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VORTEX-INDUCED-VIBRATION OF JACK-UPS WITH CYLINDRICAL LEGS IN REGULAR WAVES

机译:规则波中带有圆柱状腿的自升式涡激振动

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A simple mathematical model is developed based on the single-degree-of-freedom analogy and principle of conservation of energy evaluating various modes of Vortex-Induced-Vibration (VIV) of a jack-up with cylindrical legs in regular waves. Similar to uniform current, mass ratio, damping ratio and mode factor are found to be the important parameters controlling the cross-flow VIV and radius of gyration also for the yaw VIV. Criteria for the initiation of the mentioned VIV modes are developed for the cases of a single 2D cylinder experiencing planar oscillatory flow, four rigidly coupled 2D cylinders in rectangular configuration experiencing planar oscillatory flow and jack-up experiencing regular waves. The newly developed VIV model is validated by a set of experiments conducted in a wind, wave and current flume. The importance of mass damping parameter is further demonstrated in suppressing VIV in regular waves. The mathematical method will equip engineers to consider the effect of VIV due to regular waves in jack-up designs.
机译:基于单自由度的类比和能量守恒原理,开发了一个简单的数学模型,该模型评估了规则波状圆柱腿自升式飞机的各种涡激振动(VIV)模式。与均匀电流相似,质量比,阻尼比和模因数也是控制横流VIV和偏航VIV的重要参数,也是控制横流VIV和回转半径的重要参数。针对单个2D圆柱体经历平面振荡流,四个矩形配置的刚性耦合2D圆柱体经历平面振荡流以及自升式经历规则波的情况,提出了启动上述VIV模式的标准。新开发的VIV模型通过在风,浪和水流中进行的一系列实验得到验证。质量阻尼参数的重要性在抑制规则波中的VIV中得到了进一步证明。数学方法将使工程师能够考虑自升式设计中由于规则波动而产生的VIV的影响。

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