共查询到19条相似文献,搜索用时 140 毫秒
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提出一种基于风洞实验的风力机叶片气动负载计算方法。理论分析Beddoes-Leishman空间状态模型的非定常气动力特性,结合风洞实验数据和Beddoes-Leishman模型开发动态气动负载的数值计算程序。利用开发程序,分别详细计算DU97W300-10翼型在不同攻角区间,即线性区、失速区和全区的非定常气动系数,分析每个区间内附着流和分离流对翼型动态气动特性的影响。结果表明,在所有攻角区域的气动参数计算结果均能很好地与理论分析结果达成一致,翼型风洞实验可有效保证特定翼型动态气动负载计算的准确性。 相似文献
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基于涡尾迹方法的风力机非定常气动特性计算 总被引:2,自引:0,他引:2
给出了一种水平轴风力机三维非定常气动特性计算方法.风力机的绕流用预定涡尾迹模型确定,并引入涡核模型和考虑粘性引起的耗散效应对模型进行修正,解决了涡尾迹方法在大叶尖速比时普遍存在的计算发散问题.通过对Leishman-Beddoes动态失速模型中动态失速判据和模拟的修正,更准确计算侧偏风时风轮叶片的非定常气动响应.将三维旋转失速延迟模型与预定涡尾迹模型和动态失速模型适当耦合,从而计算包括三维旋转效应对叶片气动载荷非定常响应的影响,提高了风力机风轮和叶片非定常气动特性计算的准确度. 相似文献
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基于模糊逻辑数学方法建立了风力机动态失速模型,用于计算风力机翼型的非定常气动载荷。以风力机翼型S809为算例进行了非定常气动载荷的计算。计算结果表明:基于模糊逻辑的动态失速模型得到的预测结果与试验数据吻合良好,且比Leishman-Beddoes模型具有更高的预估精度,能够捕捉风力机翼型动态失速的细节特征,从而证明了该方法的正确性和有效性。 相似文献
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对叶素动量理论(BEM)进行改进,动量理论的计算仍在风轮坐标系下进行,而叶素理论的计算在叶片的局部坐标系下进行。在局部坐标系下能更准确地利用二维翼型的特性来计算气动载荷,同时也能更好地调用Beddoes-Leishman(B-L)模型,从而全面考虑到风轮锥角、局部风况甚至叶片弯曲变形的影响。再将动量理论和叶素理论统一在风轮坐标系下完成迭代。采用B-L模型预测二维翼型的动态气动性能时应用切向力分离点计算分离流切向力,从而提高模型对动态气动阻力的预测精度。结合改进的BEM理论和动态效应模型对Tjaereborg 2 MW风力机进行仿真,所得叶根挥舞弯矩相比经典BEM更接近测试值。 相似文献
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Horizontal axis wind turbines (HAWTs) experience three‐dimensional rotational and unsteady aerodynamic phenomena at the rotor blades sections. These highly unsteady three‐dimensional effects have a dramatic impact on the aerodynamic load distributions on the blades, in particular, when they occur at high angles of attack due to stall delay and dynamic stall. Unfortunately, there is no complete understanding of the flow physics yet at these unsteady 3D flow conditions, and hence, the existing published theoretical models are often incapable of modelling the impact on the turbine response realistically. The purpose of this paper is to provide an insight on the combined influence of the stall delay and dynamic stall on the blade load history of wind turbines in controlled and uncontrolled conditions. New dynamic stall vortex and nonlinear tangential force coefficient modules, which integrally take into account the three dimensional rotational effect, are also proposed in this paper. This module along with the unsteady influence of turbulent wind speed and tower shadow is implemented in a blade element momentum (BEM) model to estimate the aerodynamic loads on a rotating blade more accurately. This work presents an important step to help modelling the combined influence of the stall delay and dynamic stall on the load history of the rotating wind turbine blades which is vital to have lighter turbine blades and improved wind turbine design systems. 相似文献
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风力机叶片动态失速时的非定常气动特性及严重的迟滞现象使得风力机功率实测值严重偏离其静态预测值。鉴于此,基于Theodorsen理论、基尔霍夫势流理论,在忽略低阶附加质量引起的下洗气流加速度项及状态变量转换后,提出一种包括翼型附着流和后缘动态分离流的新型动态失速模型。利用该模型分析NREL 5 MW海上风力机叶片6种翼型的非定常动态失速特性得出:通过翼型的气流在完全附着流与完全分离流之间不断转换,受附着流脱落尾诱导的动态下洗气流影响及边界层动态分离产生的压力滞后的双重作用,动态升力系数变化曲线和静态升力现象曲线偏差较大,6种翼型动态升力系数变化曲线均呈非常明显的迟滞环现象。DU40、DU35、DU30、DU25、DU21和NACA64这6种翼型动态升力系数增幅明显,分别达17.6%、60.9%、60.7%、55.1%、63.7%和40.8%。动态失速攻角极大地超过静态失速攻角,分别增大到36.53°、21.40°、20.20°、17.68°、16.97°和21.42°。6种翼型动态失速预测结果与公开实验数据结论一致,证实所提出的动态失速气动模型计算结果准确可信,具有较强通用性。 相似文献
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The aim of this study is to assess the load predicting capability of a classical Beddoes–Leishman dynamic stall model in a horizontal axis wind turbine environment, in the presence of yaw misalignment. The dynamic stall model was tailored to the horizontal axis wind turbine environment and validated against unsteady thick airfoil data. Subsequently, the dynamic stall model was implemented in a blade element‐momentum code for yawed flow, and the results were compared with aerodynamic measurements obtained in the MEXICO (Model Rotor Experiments under Controlled Conditions) project on a wind turbine rotor placed in a large scale wind tunnel. In general, reasonable to good agreement was found between the blade element‐momentum model and MEXICO data. When large yaw misalignments were imposed, poor agreement was found in the downstroke of the movement between the model and the experiment. Still, over a revolution, the maximum normal force coefficient predicted was always within 8% of experimental data at the inboard stations, which is encouraging especially when blade fatigue calculations are being considered. Copyright © 2012 John Wiley & Sons, Ltd. 相似文献
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An analysis of dynamic stall for the S809 aerofoil has been performed in conjunction with the Leishman–Beddoes dynamic stall model that was modified for wind turbine applications. Numerical predictions of the lift, drag and pitching moment coefficients were compared with measurements obtained for an oscillating S809 aerofoil at various reduced frequencies, mean angles of attack and angle of attack amplitudes. It was found that the results using the modified model were in good agreement with the experimental data. Hysteresis in the aerodynamic coefficients was captured well, although the drag coefficient was slightly underpredicted in the deep stall flow regime. Validation against the experimental data showed overall good agreement. The mathematical structure of the model is such that it can be readily incorporated into a comprehensive analysis code for a wind turbine. Copyright © 2006 John Wiley & Sons, Ltd. 相似文献
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The aerodynamic loads for MW scale horizontal-axis wind turbines are calculated and analyzed in the established coordinate systems which are used to describe the wind turbine. In this paper, the blade element momentum (BEM) theory is employed and some corrections, such as Prandtl and Buhl models, are carried out. Based on the B-L semi-empirical dynamic stall (DS) model, a new modified DS model for NACA63-4xx airfoil is adopted. Then, by combing BEM modified theory with DS model, a set of calculation method of aerodynamic loads for large scale wind turbines is proposed, in which some influence factors such as wind shear, tower, tower and blade vibration are considered. The research results show that the presented dynamic stall model is good enough for engineering purpose; the aerodynamic loads are influenced by many factors such as tower shadow, wind shear, dynamic stall, tower and blade vibration, etc, with different degree; the single blade endures periodical changing loads but the variations of the rotor shaft power caused by the total aerodynamic torque in edgewise direction are very small. The presented study approach of aerodynamic loads calculation and analysis is of the university, and helpful for thorough research of loads reduction on large scale wind turbines. 相似文献
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Turbine aerodynamics remains a challenging and crucial research area for wind energy. Blade aerodynamic forces responsible for power production must be augmented to maximize energy capture. At the same time, adverse aerodynamic loads that fatigue turbine components need to be mitigated to extend machine service life. Successful resolution of these conflicting demands and continued cost of energy reduction require accurate blade aerodynamic models. This, in turn, depends on clear physical understanding and reliable numerical modeling of rotational augmentation and dynamic stall, the two phenomena principally responsible for amplified turbine blade aerodynamic loads. The current work examines full-scale turbine blade aerodynamic measurements and current modeling methodologies to better understand the physical and numerical attributes that determine model performance 相似文献