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Numerical investigation into the effect of the trailing edge shape on added mass and hydrodynamic damping for a hydrofoil

机译:尾缘形状对水翼添加肿块和流体动力阻尼效果的数值研究

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Engineering applications prove that the modification of the trailing edge shape of a blade can effectively reduce the amplitude of the vortex-induced vibration, but the mechanism behind it is still not fully understood. In this investigation, unsteady CFD and two-way FSI numerical simulation methods are performed on three-dimensional (3D) NACA 0009 hydrofoils with blunt and Donaldson trailing edges. The vortex shedding formation process, the added mass and the hydrodynamic damping ratio at different flow velocities are investigated. The relative deviations in the vortex shedding frequency, the natural frequency in water, and the hydrodynamic damping ratio obtained by simulation are within 12.88%, 4.62% and 8.82%, respectively, compared with the experimental results. As the flow velocity increases, the added mass for blunt and Donaldson trailing edge hydrofoils remains almost constant and gradually decreases, respectively. The hydrodynamic damping ratio of the hydrofoil increases linearly as the flow velocity increases with both blunt and Donaldson trailing edges involving a slope of 0.0032 and 0.005, respectively. At a flow velocity of 20 m/s, the maximum amplitude is reduced to 57% after Donaldson trailing edge modification. The results show that the hydrodynamic damping ratio of the Donaldson trailing edge is significantly increased when the flow velocity is greater than 20 m/s. The reason for this is the collision between the upper and lower trailing edge vortexes, which leads to the faster dissipation of vortex intensity. (C) 2019 Elsevier Ltd. All rights reserved.
机译:工程应用证明,刀片的后缘形状的改变可以有效地降低涡旋诱导的振动的幅度,但是其背后的机制仍然没有完全理解。在本研究中,在具有钝器和唐纳森尾部的三维(3D)Naca 0009水翼上执行不稳定的CFD和双向FSI数值模拟方法。研究了涡旋脱落的形成过程,增加了不同流速下的质量和流体动力阻尼比。与实验结果相比,涡旋脱落频率,水中的自然频率和水中的水动力阻尼比的相对偏差分别在12.88%,4.62%和8.82%以内。随着流速增加,钝器和唐纳森后缘水翼膜的添加质量分别几乎恒定并且逐渐减小。随着流速增加,水膜的流体动力阻尼比随着延迟和唐纳森尾部的延迟分别增加,涉及0.0032和0.005的斜率。在20米/秒的流速下,唐纳森后缘修改后,最大幅度降低至57%。结果表明,当流速大于20米/秒时,唐纳森后缘的流体动力阻尼比显着增加。其原因是上下后缘涡旋之间的碰撞,这导致涡旋强度的速度迅速耗散。 (c)2019年elestvier有限公司保留所有权利。

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