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首页> 外文期刊>Journal of Fluids and Structures >Coherent and turbulent process analysis of the effects of a longitudinal vortex on boundary layer detachment on a NACA0015 foil
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Coherent and turbulent process analysis of the effects of a longitudinal vortex on boundary layer detachment on a NACA0015 foil

机译:NACA0015箔上纵向涡旋对边界层分离的影响的连贯和湍流过程分析

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摘要

In this paper, the influence of a single tip vortex on boundary layer detachment is studied. This study offers a preliminary approach in order to better understand the interaction between a propeller hub vortex and the rudder installed in its wake. This configuration belongs to the field of marine propulsion and encompasses such specific problem as cavitation inception, modification of propulsive performances and induced vibrations. To better understand the complex mechanisms due to propeller-rudder interactions it was decided to emphasize configurations where the hub vortex is generated by an elliptical 3-D foil and is located upstream of a 2-D NACA0015 foil at high incidences for a Reynolds number of 5 × 10~5. The physical mechanisms were studied using Time Resolved Stereoscopic Particle Image Velocimetry (TR-SPIV) techniques. Particular attention was paid to the detachment at 25° incidence and a detailed cartography of the mean and turbulent properties of the wake is presented. Proper Orthogonal Decomposition (POD) analysis was applied in order to highlight the unsteady nature of the flow using phase averaging based on the first POD coefficients to characterize the turbulent and coherent process in the near wake of the rudder.
机译:本文研究了单尖旋涡对边界层脱离的影响。这项研究提供了一种初步方法,以便更好地了解螺旋桨毂涡流与安装在其尾流中的舵之间的相互作用。这种构造属于船舶推进领域,并且包括诸如汽蚀开始,推进性能的改变和引起的振动之类的特定问题。为了更好地理解由于螺旋桨-舵相互作用而产生的复杂机制,我们决定着重强调以下构造:轮毂涡旋由椭圆形3-D箔产生,并以高雷诺数位于2-D NACA0015箔上游。 5×10〜5。使用时间分辨立体粒子图像测速(TR-SPIV)技术研究了物理机制。特别注意了在25°入射角时的分离,并给出了尾流的平均和湍流特性的详细制图。进行适当的正交分解(POD)分析是为了使用基于第一POD系数的相平均来突出流动的不稳定特性,以表征方向舵近尾处的湍流和相干过程。

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