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A nonlinear wake model of a wind turbine considering the yaw wake steering
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作者 Yunzhou LI Zhiteng GAO +2 位作者 Shoutu LI Suiping QI Xiaoyu TANG 《Journal of Oceanology and Limnology》 SCIE CAS 2024年第3期715-727,共13页
Duo to fluctuations in atmospheric turbulence and yaw control strategies,wind turbines are often in a yaw state.To predict the far wake velocity field of wind turbines quickly and accurately,a wake velocity model was ... Duo to fluctuations in atmospheric turbulence and yaw control strategies,wind turbines are often in a yaw state.To predict the far wake velocity field of wind turbines quickly and accurately,a wake velocity model was derived based on the method of momentum conservation considering the wake steering of the wind turbine under yaw conditions.To consider the shear effect of the vertical incoming wind direction,a two-dimensional Gaussian distribution function was introduced to model the velocity loss at different axial positions in the far wake region based on the assumption of nonlinear wake expansion.This work also developed a“prediction-correction”method to solve the wake velocity field,and the accuracy of the model results was verified in wake experiments on the Garrad Hassan wind turbine.Moreover,a 33-kW two-blade horizontal axis wind turbine was simulated using this method,and the results were compared with the classical wake model under the same parameters and the computational fluid dynamics(CFD)simulation results.The results show that the nonlinear wake model well reflected the influence of incoming flow shear and yaw wake steering in the wake velocity field.Finally,computation of the wake flow for the Horns Rev offshore wind farm with 80 wind turbines showed an error within 8%compared to the experimental values.The established wake model is less computationally intensive than other methods,has a faster calculation speed,and can be used for engineering calculations of the wake velocity in the far wakefield of wind turbines. 展开更多
关键词 far wake wake model wake steering wind shear wind farm
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圆柱绕流远场旋涡结构的数值研究 被引量:8
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作者 吴文权 居江宁 《工程热物理学报》 EI CAS CSCD 北大核心 2001年第S1期17-20,共4页
基于离散涡方法求解非定常、不稳定流场。数值模拟了高雷诺数下圆柱绕流旋涡结构的发展。从流谱图、等涡量线图和涡谱图可以清晰地看出从近场初生的卡门涡街,过渡到远场的二次涡街的过程。计算结果发现:远场离散涡有形成 二个涡的涡... 基于离散涡方法求解非定常、不稳定流场。数值模拟了高雷诺数下圆柱绕流旋涡结构的发展。从流谱图、等涡量线图和涡谱图可以清晰地看出从近场初生的卡门涡街,过渡到远场的二次涡街的过程。计算结果发现:远场离散涡有形成 二个涡的涡对及三个涡的涡对结构的趋势。计算结果说明了流体运动中涡对结构的本质:远场形成的二次涡对及卡门涡街是由于流动本身的动力不稳定而引起的,从而增加对远场尾迹流及涡对结构的理解。 展开更多
关键词 涡结构 尾迹远场 离散涡方法
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公交车的远卡自动收费系统设计 被引量:1
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作者 高承 王正彦 解亚南 《单片机与嵌入式系统应用》 2015年第2期75-78,共4页
在对公交收费系统的发展和无线射频识别技术进行研究的基础上,分析了现行公交收费系统的优缺点与局限性,并提出了一种公交车远卡自动收费系统的设计思路。主要使用ARM核芯片STM32、射频芯片nRF24LE1等器件,完成了硬件设计。在软件设计... 在对公交收费系统的发展和无线射频识别技术进行研究的基础上,分析了现行公交收费系统的优缺点与局限性,并提出了一种公交车远卡自动收费系统的设计思路。主要使用ARM核芯片STM32、射频芯片nRF24LE1等器件,完成了硬件设计。在软件设计上实现了自动计算票价的扣费机制。该系统创新性地将远距离射频技术应用在公交收费系统中,不仅方便了乘客,而且大大提高了乘客上下车的效率。 展开更多
关键词 射频 远卡自动收费 STM32 唤醒电路
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A new vortex sheet model for simulating aircraft wake vortex evolution 被引量:4
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作者 Mengda LIN Guixiang CUI Zhaoshun ZHANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2017年第4期1315-1326,共12页
A new vortex sheet model was proposed for simulating aircraft wake vortex evolution.Rather than beginning with a pair of counter-rotating cylindrical vortices as in the traditional models, a lift-drag method is used t... A new vortex sheet model was proposed for simulating aircraft wake vortex evolution.Rather than beginning with a pair of counter-rotating cylindrical vortices as in the traditional models, a lift-drag method is used to initialize a vortex sheet so that the roll-up phase is taken into account. The results of this model report a better approximation to a real situation when compared to the measurement data. The roll-up induced structures are proved to influence the far-field decay.On one hand, they lead to an early decay in the diffusion phase. On the other hand, the growth of linear instability such as elliptical instability is suppressed, resulting in a slower decay in the rapid decay phase. This work provides a simple and practicable model for simulating wake vortex evolution, which combines the roll-up process and the far-field phase in simulation. It is also proved that the roll-up phase should not be ignored when simulating the far-field evolution of an aircraft wake vortex pair, which indicates the necessity of this new model. 展开更多
关键词 Aircraft Aerodynamics Large eddy simulation Vortex sheet wake vortex far field decay
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