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The Influence of Edge Sharpness on the Heave Damping Forces Experienced by a TLP Column

机译:边缘清晰度对TLP柱承受升沉阻尼力的影响

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Previous numerical investigations conducted by authors have found that two different regimes of heave damping forces experienced by a TLP column during "springing vibration" generally exist depending on Keulegan Carpenter number and frequency parameter range. Significant effect of a small corner radius (2percent of cylinder radius) at the cylinder bottom edge on the form drag has been found for a fixed oscillatory frequency (0.41 Hz) over the Keulegan Carpenter number range investigated. The present paper has further investigated the effects of the corner radius of a TLP column on the springing damping forces. It is found that the corner radius in general reduces the form drag exertedon the oscillatory cylinder, and the reduction is larger as corner radius increases. Two diffeent heave damping regimes (linear and non-linear) also exist, and the transition from linear to nonlinear damping regime is delayed due to the corner radius at the cylinder bottom edge.
机译:作者先前进行的数值研究发现,根据Keulegan Carpenter数和频率参数范围,通常存在TLP柱在“弹跳振动”过程中经历的两种不同的升沉阻尼力状态。在所研究的Keulegan Carpenter数范围内,对于固定的振荡频率(0.41 Hz),已经发现在圆柱体底部边缘处的小圆角半径(圆柱体半径的2%)对模板阻力的显着影响。本文进一步研究了TLP柱的拐角半径对弹簧阻尼力的影响。已经发现,拐角半径通常减小了施加在振动圆柱体上的形式阻力,并且随着拐角半径的增加,减小的幅度更大。还存在两种不同的升沉阻尼方式(线性和非线性),并且由于气缸底边缘的转角半径,从线性阻尼方式到非线性阻尼方式的转换被延迟。

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