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首页> 外文期刊>Mathematical Problems in Engineering: Theory, Methods and Applications >Experimental and Numerical Study on Hydrodynamic Performance of an Underwater Glider
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Experimental and Numerical Study on Hydrodynamic Performance of an Underwater Glider

机译:水下滑翔机水动力性能的实验性和数值研究

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摘要

The hydrodynamic coefficients are important parameters for predicting the motion of the glider and upgrading the hull design. In this paper, based on the Reynolds number similarity theory, 6 degrees of freedom (DOFs) of the fluid force and torque of a 11 full-scale glider model are measured. The present measurements were carried out at (2 14m/s) by varying attack angles and sideslip angles (-9 9°), respectively. The measurements were used to study the variation of the hydrodynamics of the glider, and the measurements have also been used to validate results obtained from a CFD code that uses RNG . The hydrodynamic force coefficients obtained from CFD accord well with the measurements. However, the torque coefficients difference is fairly large. Dynamics simulation results show that CFD results can be used to design and study the motion characteristics of gliders. In order to simplify the design process of gliders, we fit the empirical formula based on the experimental data and obtain a drag coefficient equation with Reynolds number. The influence of two kinds of appendages of the Conductance-Temperature-Depth (CTD) unit and thruster unit on the glider drag were studied by a contrast test. The analysis results can provide reference for design and the motion investigate of gliders.
机译:流体动力系数是用于预测滑翔机的运动并升级船体设计的重要参数。本文基于雷诺数相似理论,测量了6个流体力的6度自由(DOF)和11个全尺寸滑翔机模型的扭矩。通过分别改变攻击角和侧滑角(-9 9°),在(2 14m / s)处进行本测量。测量用于研究滑翔机的流体动力学的变化,并且还用于验证从使用RNG的CFD代码获得的结果。从CFD获得的流体动力学系数与测量相吻合。然而,扭矩系数差异相当大。动力学仿真结果表明,CFD结果可用于设计和研究滑翔机的运动特性。为了简化滑翔机的设计过程,我们根据实验数据拟合经验公式,并获得雷诺数的拖动系数方程。通过对比度测试研究了两种电导温度 - 深度(CTD)单元和推进器单元对滑翔机阻力的影响。分析结果可以为滑翔机提供设计和运动调查。

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