首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >EXTENSION OF AN UNSTEADY HYBRID NAVIER-STOKES/VORTEX-PANEL SOLVER TO WIND TURBINE AERODYNAMIC SIMULATIONS AT HIGHER YAW ANGLES
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EXTENSION OF AN UNSTEADY HYBRID NAVIER-STOKES/VORTEX-PANEL SOLVER TO WIND TURBINE AERODYNAMIC SIMULATIONS AT HIGHER YAW ANGLES

机译:扩展非稳态混合航海/涡旋-平板解算器以在更高偏航角上进行风轮机气动模拟

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A new analysis tool, an unsteady Hybrid Navier-Stokes/Vortex model, for a horizontal axis wind turbine (HAWT) has been developed for yawed flow by coupling a prescribed wake Vortex Line Method (VLM) with an unsteady Navier-Stokes solver, and its convergence and computational cost have been studied for 10 and 20 degrees of yaw. In this study, a steady viscous solution of a hybrid method is compared in detail with a full-scale Navier-Stokes simulation as a validation. Furthermore, the unsteady hybrid solver is applied to the NREL Unsteady Aerodynamics Experiment (UAE) Phase VI rotor. A test case under 10 degrees of yaw shows that the global power output agrees well with the NREL experiment, and 10 cycles of computation require less than three days using a work station under a serial CPU simulation. The same simulation performed using a super computer is used as reference, and it is estimated that the equivalent case can be obtained about 8 times faster using the work station with the present method, while keeping the same level of accuracy, than a full-domain Navier-Stokes simulation. To treat high yaw cases, new distorted prescribed vortex sheets are modeled with the VLM code. To see the difference between the base helix and the distorted helicoidal wake, unsteady hybrid VLM/Navier-Stokes solutions are examined for selected azimuth angles, and results are contrasted to a free wake BEM and NREL experimental data. For low yaw angles, the base helix approximation agrees well with the distorted helix, and yield better prediction than a free wake model, whereas for high yaw angles of more than 30 degrees, the present distorted wake gave a lower estimation of rotor torque than the free wake solver.
机译:通过将规定的尾流涡旋线法(VLM)与不稳定的Navier-Stokes求解器耦合,已开发出一种新的分析工具,即用于横轴风力涡轮机(HAWT)的不稳定的Navier-Stokes / Vortex混合模型,用于偏航。已针对10度和20度偏航角研究了其收敛性和计算成本。在这项研究中,将混合方法的稳定粘性解决方案与全尺寸Navier-Stokes仿真进行了详细比较,以进行验证。此外,非稳态混合求解器已应用于NREL非稳态空气动力学实验(UAE)的VI期转子。在偏航度为10度的情况下的测试案例表明,总功率输出与NREL实验非常吻合,并且在串行CPU模拟下使用工作站,需要10个周期的计算,不到三天。使用超级计算机执行的相同模拟被用作参考,并且估计使用本方法的工作站可以以大约8倍的速度获得等效情况,同时保持相同水平的精度,而全域Navier-Stokes模拟。为了处理偏航较大的情况,使用VLM代码对新变形的规定涡流片进行建模。为了查看基本螺旋和扭曲的螺旋尾流之间的差异,检查了选定方位角的不稳定VLM / Navier-Stokes混合解决方案,并将结果与​​自由尾流BEM和NREL实验数据进行了对比。对于低偏航角,基本螺旋近似值与扭曲的螺旋线非常吻合,并且比自由尾流模型产生更好的预测,而对于大于30度的偏航角,当前的偏航角给出的转子转矩估计值比自由偏航模型低。免费的唤醒求解器。

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