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首页> 外文期刊>Computers & Fluids >Compressible Navier-Stokes analysis of an oscillating wing in a power-extraction regime using efficient low-speed preconditioning
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Compressible Navier-Stokes analysis of an oscillating wing in a power-extraction regime using efficient low-speed preconditioning

机译:使用有效的低速预处理对功率提取状态下的振荡机翼进行可压缩的Navier-Stokes分析

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摘要

A wing that is simultaneously heaving and pitching may extract energy from an oncoming air flow, thus acting as a turbine. This paper analyzes the unsteady aerodynamics of such a device by means of time-dependent laminar flow simulations performed with a research compressible finite volume Navier-Stokes solver. The study confirms the findings of another independent report that the efficiency of the power extraction of this device can be of the order of 35%, and such an efficient operating condition is characterized by a strong dynamic stall. This study is part of a wider research programme aimed at developing a general-purpose computational framework for unsteady aerodynamic and aeroacoustic wind energy engineering. In view of aeroacoustic applications, the developed flow solver uses the compressible formulation of the Navier-Stokes equations with carefully optimized low-speed preconditioning. To demonstrate the modeling capabilities, the accuracy and the high computational performance of the developed low-speed preconditioning technology, the unsteady aerodynamics of the energy-extracting device is simulated by using a computationally challenging freestream Mach number of 0.001. A mixed preconditioning strategy that maintains both the nominal accuracy and the computational efficiency of the solver also for time-dependent low-speed problems is presented. The study also assesses the impact of a semi-implicit treatment of the unsteady source term associated with the discretization of the physical time-derivative of the governing equations on the numerical stability of the explicit multigrid integration.
机译:同时起伏和俯仰的机翼可从迎面而来的气流中提取能量,从而充当涡轮机。本文通过使用研究性可压缩有限体积Navier-Stokes解算器进行的随时间变化的层流模拟,分析了这种装置的非定常空气动力学特性。该研究证实了另一份独立报告的发现,即该设备的功率提取效率可以达到35%左右,并且这种有效的工作条件具有强大的动态失速特性。这项研究是旨在为不稳定的空气动力学和空气声风能工程开发通用计算框架的广泛研究计划的一部分。考虑到航空声学的应用,开发的流量求解器使用经过精心优化的低速预处理的Navier-Stokes方程的可压缩公式。为了证明已开发的低速预处理技术的建模能力,准确性和较高的计算性能,通过使用具有计算难度的0.001自由流马赫数模拟了能量提取设备的不稳定空气动力学。提出了一种混合预处理策略,该策略还可以解决与时间有关的低速问题,同时保持标称精度和求解器的计算效率。这项研究还评估了与控制方程的物理时间导数离散化相关的不稳定源项的半隐式处理对显式多重网格积分的数值稳定性的影响。

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