首页> 外文会议>Symposium on High Speed Marine Vehicles Conference >INDUCED DRAG OF AN AMERICA'S CUP YACHT'S FIN-BULB-WINGLET: NUMERICAL AND EXPERIMENTAL INVESTIGATION
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INDUCED DRAG OF AN AMERICA'S CUP YACHT'S FIN-BULB-WINGLET: NUMERICAL AND EXPERIMENTAL INVESTIGATION

机译:诱导美国杯游艇的Fin-Bulb-Winglet的阻力:数值和实验调查

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This paper will present both numerical and experimental activities performed at DPA on the optimization of a keel system of a typical America's Cup Yacht configuration (fin-bulb-winglet). A panel code has been extensively used to find the best shape and position of winglets to be installed on a bulb, the shape of which is fixed. The bulb is in turn connected to a keel to form the complete underwater lifting system of the sailing boat. Systematic variations of winglets geometrical parameters such as span and dihedral angle as of their position along the bulb have been performed. The result of this study has allowed the selection of the best geometries to be tested in the wind tunnel on a scaled model of the complete keel. The tests have been performed in the wind tunnel belonging to the Chalmers Department of Thermo Fluid Dynamics in Sweden. Five-hole probe measurement of the wake behind the complete lifting system has been performed to assess the velocity field in the far wake. Then a specific numerical code based on the solution of the Poisson's equations has been set up to obtain the global induced drag. This code calculates induced drag using the Maskell's formula based on velocities measured in the wake. The advantage of using Maskell's formula is in the possibility to restrict the measurement area to the zone where the vorticity is different from zero.
机译:本文将在DPA进行DPA的数值和实验活动,并在典型的美国杯游艇配置(Fin-Bulb-Winglet)的龙骨系统的优化中进行。面板代码已广泛用于查找要在灯泡上安装的WINGLET的最佳形状和位置,其形状是固定的。灯泡又连接到龙骨以形成帆船的完整水下升降系统。已经执行了沿着灯泡的位置的跨越几何参数的翼线几何参数的系统变化。本研究的结果允许选择在完全龙骨的缩放模型上在风隧道中测试的最佳几何形状。该测试已经在瑞典的Chalmers Thermo流体动力学系的风洞中进行。已经进行了完整提升系统后面唤醒的五孔探头测量,以评估远处尾迹的速度场。然后,已经设置了基于泊松方程式解决方案的特定数值代码以获得全局诱导的拖动。此代码根据在唤醒中测量的速度使用Maskell的公式计算诱导拖动。使用Maskell的公式的优点在于将测量区域限制为涡流与零不同的区域。

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