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Analysis of a Hovering Rotor using UT-GENCAS: A Modified Hybrid Navier-Stokes/Free-Wake Method

机译:使用UT-GENCAS的悬停转子的分析:改进的混合Navier-Stokes /自由唤醒方法

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Analysis of rotors in hover has always been a significant challenge. The presence of strong vortices underneath the rotor requires a large amount of grid points to properly capture the vorticity and many time steps are required to reach a time-independent state. In this study, a hybrid Navier-Stokes/free-wake method is used to preserve trailing vortices with a lower grid count. In order to achieve fast steady performance solution, two wake modeling approaches are introduced. One is a free-wake model with relaxation, and the other is a constrained down-wash wake model based on Landgrebe model. In this hybrid method, Navier-Stokes and free-wake solvers are loosely coupled for fast convergence in hover. The S-76 model-scale blades with three tip designs were studied to assess current approaches. The proposed approaches showed reasonable to good correlation with measured Figure of Merit, thrust and torque data, and the impacts of tip design and tip speed variations were captured well.
机译:悬停中的转子分析一直是一个重大挑战。转子下方强烈涡旋的存在需要大量网格点才能正确捕获旋涡,并且需要许多时间步长才能达到与时间无关的状态。在这项研究中,Navier-Stokes /自由苏醒混合方法用于保留网格数量较少的尾随涡流。为了实现快速稳定的性能解决方案,引入了两种唤醒建模方法。一个是具有松弛的自由唤醒模型,另一个是基于Landgrebe模型的约束下冲唤醒模型。在这种混合方法中,Navier-Stokes解算器和自由唤醒解算器松散耦合,以便在悬停时快速收敛。研究了具有三种尖端设计的S-76模型级叶片,以评估当前的方法。所提出的方法与测得的品质因数,推力和扭矩数据之间显示出合理至良好的相关性,并且可以很好地捕获尖端设计和尖端速度变化的影响。

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