Wing body junctions in ship hydrodynamics

C. Ungureanu, C. Mocanu, Dunărea de Jos
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引用次数: 1

Abstract

Starting with First of January 2013 all ships greater than 400 gross tons must comply with design or operational energy efficiency index, in order to reduce the greenhouse emissions. From naval architect point of view the emission reduction measures can be hydrodynamic, structural, technological and operational. The hydrodynamic measures which are the first that can be taken into consideration in order to reduce the EEDI are materialized through the optimization of the hull. The Naval Architect may interfere on the bulbous bow, hydrodynamic shoulders, bulb stern, transom or appendages, the drag being then modified by reducing the wave, viscous pressure or frictional resistance com-ponents. Other way to improve the hydrodynamics of a ship is the using of the Energy Saving Devices (ESD). These are appendages mounted on the ship hull developed to improve the flow near the propeller who operates in non-uniform wake field of ship. The flow mechanism around ESD’s resumes as wing-body juncture flow problems and due to their application to the ship appendage flow, recently, they have received much attention in ship hydrodynamics. Despite its simple geometric configuration the wing-body junction flow is a very complicate flow due to the so-called horseshoe vortex system determined by the adverse pressure gradient induced by the presence of the obstacle and the three di-mensional boundary layer separations around the junction. The horseshoe vortex flow affects the drag, lift and causes a persistent lack of uniformity in the wake and is also considered as one source of the noises, vibration and unsteady inflow for the propeller.
船舶流体力学中的翼身连接
从2013年1月1日开始,所有超过400总吨的船舶必须符合设计或运营能效指标,以减少温室气体排放。从造船工程师的角度来看,减排措施可以是水动力、结构、技术和操作。为了减少EEDI,首先要考虑的水动力措施是通过优化船体来实现的。造船师可以对球茎艏、水动力肩、球茎尾、尾梁或附属物进行干涉,然后通过减少波浪、粘性压力或摩擦阻力来改变阻力。另一种改善船舶水动力的方法是使用节能装置(ESD)。这是安装在船体上的附件,用于改善船舶在非均匀尾流场中工作的螺旋桨附近的流动。ESD周围的流动机理恢复为翼体结合部流动问题,由于其在船舶附属物流动中的应用,近年来在船舶流体力学中受到了广泛的关注。翼身结合部流动虽然几何结构简单,但由于障碍物的存在和结合部周围三维边界层的分离所引起的逆压梯度所决定的所谓马蹄形涡系统,使得翼身结合部流动是一个非常复杂的流动。马蹄形涡影响着尾迹的阻力、升力和持续的不均匀性,也是螺旋桨噪声、振动和非定常进流的来源之一。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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