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Phase-averaged stereo-PIV flow field and force/moment/motion measurements for surface combatant in PMM maneuvers

机译:PMM机动中的表面战斗机的相位平均立体声PIV流场和力/矩/运动测量

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摘要

Towing-tank experiments are performed for a surface combatant as it undergoes static and dynamic planar motion mechanism maneuvers in calm water. The data includes global forces/moment/motions and phase-averaged local flow-fields, and uncertainty assessment. The geometry is DTMB model 5512, which is a 1/46.6 scale geosym of DTMB model 5415, with L = 3.048 m. The experiments are performed in a 3.048 × 3.048 × 100 m towing tank. The measurement system features a custom designed planar motion mechanism, a towed stereoscopic particle image velocimetry system, a Krypton contactless motion tracker, and a 6-component loadcell. The forces/moment and UA are conducted in collaboration with two international facilities (FORCE and INSEAN), including test matrix and overlapping tests using the same model geometry but with different scales. Quality of the data is assessed by monitoring the statistical convergence, including tests for randomness, stationarity, and normality. Uncertainty is assessed following the ASME Standards (1998 and 2005). Hydrodynamic derivatives are determined from the forces/moment data by using the Abkowitz (1966) mathematical model, with two different u27Multiple-Run (MR)u27 and u27Single-Run (SR)u27 methods. The results for reconstructions of the forces/moment indicate that usually the MR method is more accurate than the SR. Comparisons are made of the hydrodynamic derivatives across different facilities. The scale effect is small for sway derivatives, whereas considerable for yaw derivatives. Heave, pitch, and roll motions exhibit cross-coupling between the motions and forces and moment data, as expect based on ship motions theory. Hydrodynamic derivatives are compared between different mount conditions. Linear derivatives values are less sensitive to the mounting conditions, whereas the non-linear derivatives are considerably different. Phase-averaged flowfield results indicate maneuvering-induced vortices and their interactions with the turbulent boundary layer. The tests are sufficiently documented and detailed so as to be useful as benchmark EFD data for CFD validation.
机译:牵引罐实验是对表面战斗机进行的,因为它在平静的水中经历静态和动态的平面运动机制演习。数据包括全球力/时刻/动作和阶段平均的局部流场,以及不确定性评估。几何体是DTMB型号5512,它是DTMB型号5415的1/46.6级地质yem,L = 3.048米。实验是在3.048×3.048×100米牵引箱中进行的。测量系统具有定制设计的平面运动机构,牵引立体粒子图像速度系统,Krypton非接触式运动跟踪器和6分量载荷电池。力量/时刻和UA是与两个国际设施(Force和Insean)合作进行的,包括使用相同模型几何的测试矩阵和重叠测试,但具有不同的尺度。通过监测统计收敛来评估数据质量,包括随机性,有同性和正常性的测试。根据ASME标准(1998年和2005年)评估不确定性。通过使用ABKOWITZ(1966)数学模型,使用ABKOWITZ(1966)数学模型来确定流体动力学衍生物,两种不同的 U27多运行(MR) U27和 U27Single运行(SR) U27方法。力/时刻重建的结果表明,通常MR方法比SR更准确。比较由不同设施的流体动力衍生物制成。摇摆衍生物的比例效应很小,而偏航衍生物相当大。升降,俯仰和滚动动作在运动和力和力矩数据之间表现出交叉耦合,如期望基于船舶运动理论。在不同的安装条件之间比较流体动力衍生物。线性衍生物值对安装条件敏感,而非线性衍生物相当不同。相位平均流场结果表示操纵诱导的涡流及其与湍流边界层的相互作用。测试是充分记录和详细的,以便有用作为CFD验证的基准EFD数据。

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    Hyunse Yoon;

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