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A 3D flow separation model for open propellers with blunt trailing edge

机译:具有钝后边缘的开放式螺旋桨的3D流分离模型

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摘要

The panel method is widely used in the design and analysis of marine propellers. However, this method cannot handle propellers with a blunt trailing edge due to a lack of proper models for the flow separation downstream. In this study, a numerical scheme, i.e., the three-dimensional flow separation model, is proposed to enable the panel method to be applied to propellers with a blunt trailing edge. In this model, the flow separation zone is represented as an extension of the trailing edge. The criteria of zero local lifts and zero local moments over the extension of all blade sections are used to establish the equations that determine the shape of the flow separation zone. Those equations are solved either by the Newton-Raphson method or as an optimization problem. A low-order panel method coupled with a boundary layer solver (the viscous/inviscid interaction method) is used to predict the pressure distributions and forces for the extended geometry. To validate this model, the pressure distributions of the propeller blade are compared with those from solving the Reynolds-Averaged Navier-Stokes equations. The predicted open water characteristics of a controllable pitch propeller are compared with the experimental measurements at a wide range of advance ratios with different pitches. This model requires much less computational effort while preserving high accuracy, and thus can be used reliably in designing and analyzing propellers with a blunt trailing edge.
机译:面板法广泛应用于海洋螺旋桨的设计和分析。然而,由于在下游流动分离的缺乏适当的模型,这种方法不能处理具有钝后缘的螺旋桨。在该研究中,提出了一种数值方案,即三维流动分离模型,以使面板方法能够用钝的后缘施加到螺旋桨上。在该模型中,流动分离区表示为后缘的延伸。在所有刀片部分的延伸部分上的零局部升降和零局部矩的标准用于建立确定流分离区形状的等式。这些方程由牛顿-Raphson方法或作为优化问题解决。与边界层求解器(粘性/不用相互作用方法)耦合的低阶面板方法用于预测扩展几何形状的压力分布和力。为了验证该模型,将螺旋桨叶片的压力分布与求解雷诺平均的Navier-Stokes方程的压力分布进行比较。将可控间距螺旋桨的预测开放水特性与具有不同间距的广泛预先比率的实验测量进行比较。该模型需要更少的计算工作,同时保持高精度,因此可以可靠地使用和分析具有钝后缘的螺旋桨。

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