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Effect of turbulence models on RANS computation of propeller vortex flow

机译:湍流模型对螺旋桨涡流RANS计算的影响

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The steady-state tip vortex flow of a David Taylor Model Basin (DTMB) propeller model has been computed using a RANS solver on a spiral-like structured grid with grid concentration aligned with the vortex core. Sensitivity of the numerical solutions to grid resolutions and distributions was studied. To investigate the effect of turbulence models on the predicted tip vortex flow and the open-water performance, a number of eddy viscosity turbulence models and Reynolds-stress models were used in combination with various grids. The computed velocities across the tip vortex core and their fluctuations at near field, the circumferentially averaged velocities outside the tip vortex region, and the thrust and torque coefficients were compared with experimental data. The results of error analysis are presented. It was found that the eddy viscosity turbulence models are slightly better in predicting the near field tip vortex flow and the thrust/torque coefficients than the Reynolds stress models. The effect of the grid resolution and distribution and turbulence models on the circumferentially averaged velocities outside the tip vortex region is minimal.
机译:戴维泰勒模型盆地(DTMB)螺旋桨模型的稳态尖端涡流已使用RANS求解器在螺旋状结构化网格上进行了计算,网格浓度与涡流核对齐。研究了网格分辨率和分布的数值解的敏感性。为了研究湍流模型对预测的叶尖涡流和开水性能的影响,将许多涡流粘度湍流模型和雷诺应力模型与各种网格结合使用。将计算得出的整个尖端涡流速度及其在近场处的波动,尖端涡流区域外部的周向平均速度以及推力和扭矩系数与实验数据进行了比较。给出了错误分析的结果。已发现,涡流粘度湍流模型在预测近场尖端涡流和推力/扭矩系数方面比雷诺应力模型稍好。网格分辨率,分布和湍流模型对尖端涡流区域之外的圆周平均速度的影响最小。

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