轴向板条对海洋立管涡激振动抑振的数值研究

涡激振动是一种在海洋工程领域普遍存在的流固耦合物理现象,易导致海洋立管等结构物发生疲劳损伤或失稳。本文为抑制涡激振动而提出一种附加轴向板条的方案,采用非定常流体数值计算方法求解分析不同分布形式下的轴向板条对海洋立管涡激振动特性的影响。首先定义轴向板条的分布形式;采用Newmark-β法求解立管双自由度振动方程并编写UDF,计算采用k-ω/SST湍流模型,并结合动网格技术模拟立管的振动过程。研究结果表明,轴向板条对海洋立管具有较好的抑振效果;当轴向板条数目n=20时,流向振动幅度减小78.57%,横向振动幅度减小58.10%。本文研究结果可为海洋结构物涡激振动的抑振提供参考。     

荆州市豉湖渠排涝泵站工程设计

该文通过湖北省荆州市豉湖渠排涝泵站工程,介绍了该泵站规模的确定、站址的选择、工程布置以及主要构筑物的设计,可供类似工程参考。     

Numerical Research of Flow past a Circular Cylinder with Splitter Plate at a Subcritical Reynolds Number Region

Numerical research of flow past a circular cylinder with a splitter at the subcritical Reynolds number region of 5 × 10~4—9 × 10~4 was researched based on Computational Fluid Dynamics(CFD) through solving twodimensional incompressible unsteady Reynolds-averaged Navier-Stokes(URANS) equations with the shear stress transport(SST) k-ω turbulence model. Three different grid resolutions were employed in the verification and validation study of the adopted turbulence model. Various fluid characteristics such as Strouhal number, lift coefficient of the cylinder and the splitter with respect to various splitter lengths and different Reynolds numbers were investigated. It was revealed that the lift coefficient ratio of the splitter over the cylinder remains near 1.6 when the splitter length is 1.5—4 times the cylinder's diameter. Vortex shedding is strongly inhibited when the splitter length is greater than a critical value of around four times the cylinder's diameter. The phase difference of the lift coefficient on the upper and lower surface of the splitter varies between-30?and 30?. The maximal lift coefficients are reached when the splitter length is about 2 times the cylinder's diameter. Besides, the splitter length has little influence on the separation angle around the cylinder.     

Development trend and key technologies of autonomous underwater vehicles北大核心CSCD

为推进和引导我国自主水下航行器(AUV)的发展,总结国内外AUV的研究现状,提出其系列化、集群化、体系化、大型化的发展趋势。重点探讨AUV总体多学科优化设计、结构与材料设计、动力与推进、导航与控制、探测与通信等关键技术,为更好地利用AUV经略海洋,从而实现“进入海洋、探测海洋、利用海洋”的战略目标提出发展意见。     

旋转翼对海洋立管涡激振动抑振的数值研究

为抑制海洋立管的涡激振动,本文提出一种安装旋转翼的方案.采用非定常数值计算方法求解分析常规海洋立管和安装有旋转翼海洋立管的涡激振动特性.对旋转翼的相关参数进行定义;建立立管单自由度振动模型,并采用Newmark-β法数值求解振动方程;编写CFD数值计算的UDF,并结合动网格技术模拟求解立管的涡激振动过程.结果表明:随着旋转翼旋转角速度的增加,立管的振幅比逐渐减小,最后基本不变,抑制振动效果十分明显;当旋转角速度ω=3.0 rad/s时,旋转翼的控制效果最优,振幅比从0.98下降到0.008,振幅比降低99.2％;旋转翼的旋转运动会破坏海洋立管脱落的尾流漩涡,从而破坏海洋立管的周期性振动.