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Experimental Investigation on Lift Coefficient for a Truss SPAR Subjected to Vortex Induced Motions

机译:桁架翼料升力系数对涡旋诱导运动的实验研究

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The prediction of lift coefficient of Truss Spars is the base for investigating added mass coefficient and damping coefficient, which are important in the estimation of fatigue damage rates. The 1:60 scale Truss Spar model tests have been conducted in towing tank at Zhejiang Ocean University (ZOU). The Truss Spar model consists of a hard tank with removable helical strakes, a truss section and a square soft tank. Model tests were carried out with simplified mooring system. In this study, results from the experiment subjected to uniform current were reported. The Reynolds numbers varied from 8E04 to 2E05. The lift coefficient, lift coefficient components in phase with velocity and acceleration and the phase angle were calculated. The results showed that the symbol of the lift coefficient in phase with velocity varied with the reduced velocity, while the lift coefficient in phase with acceleration was negative at the investigated range of reduced velocity. The magnitude of lift coefficient in phase with acceleration decided the magnitude of the lift coefficient. The symbol of phase angle varied with the reduced velocity, which was in agreement with the symbol of the lift coefficient in phase with velocity.
机译:桁架翼梁升力系数的预测是研究增加质量系数和阻尼系数的基础,这在疲劳损伤率的估计中是重要的。 1:60规模桁架翼乐模型试验已在浙江海洋大学(ZOU)牵引箱进行。 Truss Spar模型由一个带有可移动螺旋轨迹的硬罐,桁架部分和方形软罐。模型测试是用简化的系泊系统进行的。在该研究中,报告了经受均匀电流的实验结果。雷诺数从8E04到2E05变化。计算升力系数,升力系数分量与速度和加速度和相位角的相位。结果表明,随着速度的速度变化的速度变化的升力系数的象征,而在调查范围的速度下,升力与加速度的升力系数为负。随着加速的升力系数的大小决定了提升系数的大小。相位角的符号随着速度的降低而变化,其与具有速度相位的升力系数的象征一致。

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