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A simple vortex model applied to an idealized rotor in sheared inflow 一个应用于剪切流入中理想化转子的简单涡流模型
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-04-06 DOI: 10.5194/wes-8-503-2023
Abstract. A simple analytical vortex model is presented and used to study an idealized wind turbine rotor in uniform and sheared inflow, respectively.Our model predicts that 1D momentum theory should be applied locally when modelling a non-uniformly loaded rotor in a sheared inflow. Hence the maximum local power coefficient (expressed with respect to the local, upstream velocity) of an ideal rotor is not affected by the presence of shear. We study the interaction between the wake vorticity generated by the rotor and the wind shear vorticity and find that their mutual interaction results in no net generation of axial vorticity: the wake effects and the shear effects exactly cancel each other out. This means that there are no resulting cross-shear-induced velocities and therefore also no cross-shear deflection of the wake in this model.
摘要提出了一个简单的涡流分析模型,并分别用于研究理想化的风机转子在均匀流和剪切流中的涡流。我们的模型预测,当对剪切流入中的非均匀加载转子进行建模时,应局部应用1D动量理论。因此,理想转子的最大局部功率系数(相对于局部上游速度表示)不受剪切的影响。我们研究了转子产生的尾流涡度和风切变涡度之间的相互作用,发现它们的相互作用导致轴涡度没有净产生:尾流效应和切变效应正好相互抵消。这意味着在该模型中没有产生横向剪切诱导速度,因此也没有尾流的横向剪切偏转。
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引用次数: 0
Investigations of correlation and coherence in turbulence from a large-eddy simulation 从大涡模拟研究湍流的相关性和相干性
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-04-06 DOI: 10.5194/wes-8-487-2023
Regis Thedin, E. Quon, M. Churchfield, P. Veers
Abstract. Microscale flow descriptions are often given in terms of mean quantities, turbulent kinetic energy, and/or stresses. Those metrics, while valuable, give limited information about turbulent eddies and coherent turbulent structures. This work investigates the structure of an atmospheric boundary layer using coherence and correlation in space and time with a range of separation distances. We calculate spatial correlations over entire planes of velocity fluctuations, from which we can evaluate the correlation along different directions at different spacings. Similarly, coherence of the three velocity components over separations in the three directions is also investigated. We apply these analyses to a mesoscale–microscale coupled scenario with time-varying conditions and examine nuances in spatial correlations that are often overlooked. Through these analyses and results, this work highlights important differences observed in terms of coherence when comparing large-eddy simulation data to simpler models and suggests ways to improve these simpler models. We note that such differences are important for disciplines like wind energy structural dynamic analysis, in which blade loading and fatigue depend strongly on the structure of the turbulence. We emphasize the additional wealth of data that can be provided by typical atmospheric boundary layer large-eddy simulation when correlation and coherence analysis is included, and we also state the limitations of large-eddy simulation data, which inherently truncate the smaller scales of turbulence.
摘要微观尺度的流动描述通常是根据平均量、湍流动能和/或应力给出的。这些指标虽然有价值,但对湍流涡流和连贯湍流结构提供的信息有限。本文利用空间和时间上的相干性和相关性在一定的分离距离范围内研究了大气边界层的结构。我们计算了整个速度波动平面的空间相关性,从中我们可以评估在不同间距沿不同方向的相关性。同样,三个速度分量在三个方向上的相干性也进行了研究。我们将这些分析应用于具有时变条件的中尺度-微观耦合场景,并检查经常被忽视的空间相关性中的细微差别。通过这些分析和结果,本工作强调了将大涡模拟数据与简单模型进行比较时在相干性方面观察到的重要差异,并提出了改进这些简单模型的方法。我们注意到,这种差异对于风能结构动力分析等学科很重要,在这些学科中,叶片载荷和疲劳在很大程度上取决于湍流的结构。我们强调了当包含相关和相干分析时,典型的大气边界层大涡模拟可以提供额外的丰富数据,并且我们也说明了大涡模拟数据的局限性,它固有地截断了较小尺度的湍流。
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引用次数: 1
OC6 project Phase III: validation of the aerodynamic loading on a wind turbine rotor undergoing large motion caused by a floating support structure OC6项目第三阶段:风力发电机转子在浮式支撑结构引起的大运动下的气动载荷验证
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-04-06 DOI: 10.5194/wes-8-465-2023
R. Bergua, A. Robertson, J. Jonkman, E. Branlard, A. Fontanella, M. Belloli, P. Schito, A. Zasso, G. Persico, A. Sanvito, E. Amet, C. Brun, Guillén Campaña-Alonso, Raquel Martín-San-Román, Ruolin Cai, Jifeng Cai, Quan Qian, Wen Maoshi, A. Beardsell, G. Pirrung, N. Ramos‐García, W. Shi, J. Fu, Rémi Corniglion, A. Lovera, J. Galván, T. Nygaard, Carlos Renan dos Santos, P. Gilbert, Pierre-Antoine Joulin, F. Blondel, Eelco Frickel, Peng Chen, Zhiqiang Hu, R. Boisard, Kutay Yilmazlar, A. Croce, V. Harnois, Lijun Zhang, Ye Li, A. Aristondo, Iñigo Mendikoa Alonso, S. Mancini, K. Boorsma, F. Savenije, D. Marten, R. Soto‐Valle, C. Schulz, S. Netzband, A. Bianchini, F. Papi, S. Cioni, P. Trubat, D. Alarcón, C. Molins, M. Cormier, Konstantin Brüker, T. Lutz, Qing Xiao, Z. Deng, F. Haudin, Akhilesh Goveas
Abstract. This paper provides a summary of the work done within Phase III of the Offshore Code Comparison Collaboration, Continued, with Correlation and unCertainty (OC6) project, under the International Energy Agency Wind Technology Collaboration Programme Task 30. This phase focused on validating the aerodynamic loading on a wind turbine rotor undergoing largemotion caused by a floating support structure. Numerical models of theTechnical University of Denmark 10 MW reference wind turbine were validated using measurement data from a 1:75 scale test performed during the UNsteady Aerodynamics for FLOating Wind (UNAFLOW) project and a follow-on experimental campaign, both performed at the Politecnico di Milano wind tunnel. Validation of the models was performed by comparing the loads for steady (fixed platform) and unsteady (harmonic motion of the platform) wind conditions. For the unsteady wind conditions, the platform was forced to oscillate in the surge and pitch directions under several frequencies and amplitudes. These oscillations result in a wind variation that impacts the rotor loads (e.g., thrust and torque). For the conditions studied in these tests, the system aerodynamic response was almost steady. Only a small hysteresis in airfoil performance undergoing angle of attack variations in attached flow was observed. During the experiments, the rotor speed and blade pitch angle were held constant. However, in real wind turbine operating conditions, the surge and pitch variations would result in rotor speed variations and/or blade pitch actuations, depending on the wind turbine controller region that the system is operating. Additionalsimulations with these control parameters were conducted to verify thefidelity of different models. Participant results showed, in general, a goodagreement with the experimental measurements and the need to account fordynamic inflow when there are changes in the flow conditions due to therotor speed variations or blade pitch actuations in response to surge andpitch motion. Numerical models not accounting for dynamic inflow effectspredicted rotor loads that were 9 % lower in amplitude during rotor speedvariations and 18 % higher in amplitude during blade pitch actuations.
摘要本文总结了在国际能源署风能技术合作计划任务30下,海上代码比较合作(续)第三阶段(OC6)项目中所做的工作。本阶段的重点是验证风力涡轮机转子上的空气动力学载荷,该转子正经历由浮动支撑结构引起的大运动。丹麦科技大学的数值模型10 MW参考风力涡轮机使用1:75比例测试的测量数据进行了验证,该测试是在“漂浮风的不稳定空气动力学”(UNAFLOW)项目和后续实验活动期间进行的,这两项活动都是在米兰理工大学风洞进行的。通过比较稳定(固定平台)和非稳定(平台的谐波运动)风条件下的载荷,对模型进行了验证。对于非定常风条件,平台被迫在几个频率和振幅下沿涌浪和俯仰方向振荡。这些振荡导致风的变化,从而影响转子负载(例如,推力和扭矩)。在这些试验中研究的条件下,系统的气动响应几乎是稳定的。在附流攻角变化的情况下,只观察到翼型性能的微小滞后。在实验过程中,转子速度和叶片桨距角保持不变。然而,在实际的风力涡轮机操作条件下,喘振和变桨变化将导致转子速度变化和/或叶片变桨致动,这取决于系统正在操作的风力涡轮机控制器区域。利用这些控制参数进行了额外的仿真,以验证不同模型的有效性。参与者的结果表明,总体而言,与实验测量结果一致,并且当由于转子速度变化或叶片桨距致动而导致流动条件发生变化时,需要考虑动态流入。未考虑动态流入效应的数值模型预测转子载荷为9 % 转子转速变化时振幅较低,18 % 在叶片变桨致动期间振幅更高。
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引用次数: 11
Evolution of eddy viscosity in the wake of a wind turbine 风力涡轮机尾流中涡流粘度的演变
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-03-30 DOI: 10.5194/wes-8-449-2023
R. Scott, L. Martínez‐Tossas, J. Bossuyt, N. Hamilton, R. B. Cal
Abstract. The eddy viscosity hypothesis is a popular method in wind turbine wake modeling for estimating turbulent Reynolds stresses. We document the downstream evolution of eddy viscosity in the wake of a wind turbine from experimental and large-eddy-simulation data. Wake eddy viscosity is isolated from its surroundings by subtracting the inflow profile, and the driving forces are identified in each wake region. Eddy viscosity varies in response to changes in turbine geometry and nacelle misalignment with larger turbines generating stronger velocity gradients and shear stresses. We propose a model for eddy viscosity based on a Rayleigh distribution. Model parameters are obtained from scaling the eddy viscosity hypothesis and demonstrate satisfactory agreement with the reference data. The model is implemented in the curled wake formulation in the FLOw Redirection and Induction in Steady State (FLORIS) framework and assessed through comparisons with the previous formulation. Our approach produced more accurate flow field estimates with lower total error for the majority of cases.
摘要涡粘性假设是风力涡轮机尾流建模中用于估计湍流雷诺应力的一种流行方法。我们从实验和大涡模拟数据中记录了风力涡轮机尾流中涡粘度的下游演变。通过减去流入剖面,将尾流涡流粘度与其周围环境隔离开来,并确定每个尾流区域的驱动力。涡流粘度随涡轮机几何形状和机舱错位的变化而变化,较大的涡轮机产生更强的速度梯度和剪切应力。我们提出了一个基于瑞利分布的涡流粘度模型。模型参数是通过缩放涡流粘度假设获得的,并与参考数据证明了令人满意的一致性。该模型在稳态FLOw重定向和诱导(FLORIS)框架中的卷曲尾流公式中实现,并通过与先前公式的比较进行评估。我们的方法在大多数情况下产生了更准确的流场估计,总误差更低。
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引用次数: 2
Validation of turbulence intensity as simulated by the Weather Research and Forecasting model off the US northeast coast 美国东北海岸外天气研究与预报模式模拟的湍流强度的验证
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-03-29 DOI: 10.5194/wes-8-433-2023
S. Tai, L. Berg, R. Krishnamurthy, R. Newsom, A. Kirincich
Abstract. Turbulence intensity (TI) is often used to quantify the strength ofturbulence in wind energy applications and serves as the basis of standardsin wind turbine design. Thus, accurately characterizing the spatiotemporalvariability in TI should lead to improved predictions of power production.Nevertheless, turbulence measurements over the ocean are far less prevalentthan over land due to challenges in instrumental deployment, maintenance,and operation. Atmospheric models such as mesoscale (weather prediction) and large-eddy simulation (LES) models are commonly used in the wind energy industry to assess the spatial variability of a given site. However, the TI derivation from atmospheric models has not been well examined. An algorithm is proposed in this study to realize online calculation of TI in the Weather Research and Forecasting (WRF) model. Simulated TI is divided into two components depending on scale, including sub-grid (parameterized based on turbulence kinetic energy (TKE)) and grid resolved. The sensitivity of sea surface temperature (SST) on simulated TI is also tested. An assessment is performed by using observations collected during a field campaign conducted from February to June 2020 near the Woods Hole Oceanographic Institution Martha's Vineyard Coastal Observatory. Results show that while simulated TKE is generally smaller than the lidar-observed value, wind speed bias is usually small. Overall, this leads to a slight underestimation in sub-grid-scale estimated TI. Improved SST representation subsequently reduces model biases in atmospheric stability as well as wind speed and sub-grid TI near the hub height. Large TI events in conjunction with mesoscale weather systems observed during the studied period pose a challenge to accurately estimating TI from models. Due to notable uncertainty in accurately simulating those events, this suggests summing up sub-grid and resolved TI may not be an ideal solution. Efforts in further improving skills in simulating mesoscale flow and cloud systems are necessary as the next steps.
摘要湍流强度(TI)通常用于量化风能应用中的湍流强度,并作为风力涡轮机设计标准的基础。因此,准确地描述TI的时空变化性应该可以改善对电力生产的预测。然而,由于仪器部署、维护和操作方面的挑战,海洋湍流测量远不如陆地湍流测量普遍。中尺度(天气预测)和大涡模拟(LES)等大气模型通常用于风能行业,以评估给定场地的空间变异性。然而,从大气模型推导出的TI并没有得到很好的检验。本文提出了一种在天气研究与预报(WRF)模型中实现TI在线计算的算法。模拟TI根据尺度分为两个部分,包括子网格(基于湍流动能(TKE)进行参数化)和网格解析。还测试了海面温度对模拟TI的敏感性。评估是利用2020年2月至6月在伍兹霍尔海洋研究所玛莎葡萄园海岸天文台附近进行的实地考察中收集的观测结果进行的。结果表明,虽然模拟的TKE通常小于激光雷达的观测值,但风速偏差通常较小。总的来说,这导致了对子电网规模估计TI的轻微低估。改进的SST表示随后减少了大气稳定性以及轮毂高度附近的风速和子网格TI的模型偏差。在研究期间观测到的大型TI事件和中尺度天气系统对从模型中准确估计TI提出了挑战。由于准确模拟这些事件存在显著的不确定性,这表明总结子网格和解决的TI可能不是理想的解决方案。下一步有必要努力进一步提高模拟中尺度气流和云系统的技能。
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引用次数: 0
Assessing the rotor blade deformation and tower–blade tip clearance of a 3.4 MW wind turbine with terrestrial laser scanning 评估转子叶片变形和3.4 带地面激光扫描的MW风力涡轮机
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-03-27 DOI: 10.5194/wes-8-421-2023
Paula Helming, A. Intemann, Klaus-Peter Webersinke, A. von Freyberg, M. Sorg, A. Fischer
Abstract. Wind turbines have grown in size in recent years, makingefficient structural health monitoring of all of their structures evenmore important. Wind turbine blades deform elastically under the loadsapplied to them by wind and inertial forces acting on the rotating rotorblades. In order to properly analyze these deformations, an earthboundsystem is desirable that can measure the blade deformation, as well as thetower–blade tip clearance from a large measurement working distance of over150 m and a single location. To achieve this, a terrestrial laser scanner(TLS) in line-scanning mode with vertical alignment is used to measure thedistance to passing blades and the tower for different wind loads over time.In detail, the blade deformations for two different wind load categories areevaluated and compared. Additionally, the tower–blade tip clearance iscalculated and analyzed with regard to the rotor speed. Using a Monte Carlosimulation, the measurement uncertainty is determined to be in the millimeter rangefor both the blade deformation analysis and the tower–blade tip clearance.The in-process applicable measurement methods are applied and validated on a3.4 MW wind turbine with a hub height of 128 m. The deformation of the bladeincreases with higher wind speed in the wind direction, while the tower–bladetip clearance decreases with higher wind speed. Both relations are measurednot only qualitatively but also quantitatively. Furthermore, no differencebetween the three rotor blades is observed, and each of the three blades isshown to be separately measurable. The tower–blade tip clearance is comparedto a reference video measurement, which recorded the tower–blade tipclearance from the side, validating the novel measurement approach.Therefore, the proposed setup and methods are proven to be effective toolsfor the in-process structural health monitoring of wind turbine blades.
摘要近年来,风力涡轮机的规模越来越大,这使得对其所有结构进行有效的结构健康监测变得更加重要。风力涡轮机叶片在风力和惯性力作用于旋转转子叶片的载荷作用下弹性变形。为了正确地分析这些变形,需要一个地面系统,可以测量叶片变形,以及从150米以上的大测量工作距离和单个位置的塔-叶尖间隙。为了实现这一目标,地面激光扫描仪(TLS)采用垂直对齐的线扫描模式来测量随着时间的推移,不同风荷载与经过叶片和塔的距离。详细地,评估和比较了两种不同风荷载类别下的叶片变形。此外,计算和分析了塔叶顶间隙与转子转速的关系。通过蒙特卡罗模拟,确定了叶片变形分析和塔尖间隙的测量不确定度在毫米范围内。在一台轮毂高度为128 m的3.4 MW风力发电机组上进行了过程中适用的测量方法的应用和验证。叶片在风向上的变形随风速的增大而增大,塔叶间隙随风速的增大而减小。这两种关系不仅是定性的,而且是定量的。此外,没有不同的三个转子叶片被观察到,每一个叶片被显示是可单独测量的。将塔叶顶间隙与从侧面记录塔叶顶间隙的参考视频进行比较,验证了新测量方法。因此,所提出的设置和方法被证明是风电叶片在过程中结构健康监测的有效工具。
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引用次数: 1
Comparison of free vortex wake and blade element momentum results against large-eddy simulation results for highly flexible turbines under challenging inflow conditions 高柔性涡轮自由涡尾迹和叶片单元动量计算结果与大涡模拟结果的比较
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-03-24 DOI: 10.5194/wes-8-383-2023
K. Shaler, Benjamin Anderson, L. Martínez‐Tossas, E. Branlard, Nick Johnson
Abstract. Throughout wind energy development, there has been a push to increase wind turbine size due to the substantial economic benefits. However, increasing turbine size presents several challenges, both physically and computationally. Modeling large, highly flexible wind turbines requires highly accurate models to capture the complicated aeroelastic response due to large deflections and nonstraight blade geometries. Additionally, the development of floating offshore wind turbines requires modeling techniques that can predict large rotor and tower motion. Free vortex wake methods model such complex physics while remaining computationally tractable to perform key simulations necessary during the turbine design process. Recently, a free vortex wake model – cOnvecting LAgrangian Filaments (OLAF) – was added to the National Renewable Energy Laboratory's engineering tool OpenFAST to allow for the aerodynamic modeling of highly flexible turbines along with the aero-hydro-servo-elastic response capabilities of OpenFAST. In this work, free vortex wake and low-fidelity blade element momentum (BEM) results are compared to high-fidelity actuator-line computational fluid dynamics simulation results via the Simulator fOr Wind Farm Applications (SOWFA) method for a highly flexible downwind turbine for varying yaw misalignment, shear exponent, and turbulence intensity conditions. Through these comparisons, it was found that for all considered quantities of interest, SOWFA, OLAF, and BEM results compare well for steady inflow conditions with no yaw misalignment. For OLAF results, this strong agreement with the SOWFA results was consistent for all yaw misalignment values. The BEM results, however, deviated significantly more from the SOWFA results with increasing absolute yaw misalignment. Differences between OLAF and BEM results were dominated by the yaw misalignment angle, with varying shear exponent and turbulence intensity leading to more subtle differences. Overall, OLAF results were more consistent than BEM results when compared to SOWFA results under challenging inflow conditions.
摘要在整个风能开发过程中,由于其巨大的经济效益,一直在推动增加风力涡轮机的尺寸。然而,涡轮机尺寸的增加在物理和计算上都带来了一些挑战。建模大型、高度柔性的风力涡轮机需要高度精确的模型来捕捉由于大挠度和非直叶片几何形状而引起的复杂气动弹性响应。此外,浮动海上风力涡轮机的开发需要能够预测大型转子和塔架运动的建模技术。自由涡尾流方法对这种复杂的物理现象进行建模,同时保持计算的灵活性,以便在涡轮机设计过程中进行必要的关键模拟。最近,国家可再生能源实验室的工程工具OpenFAST中添加了一个自由涡流尾流模型——cOnvecting LAgrangian Filaments(OLAF),以实现高度柔性涡轮机的空气动力学建模以及OpenFAST的气动-液压伺服弹性响应能力。在这项工作中,通过风电场应用模拟器(SOWFA)方法,将自由涡流尾流和低保真度叶片单元动量(BEM)结果与高保真度执行器线计算流体动力学模拟结果进行了比较,该方法适用于高度柔性的下风机,用于不同的偏航偏差、剪切指数和湍流强度条件。通过这些比较,发现对于所有考虑的感兴趣的量,SOWFA、OLAF和BEM结果在没有偏航偏差的稳定流入条件下比较良好。对于OLAF结果,这种与SOWFA结果的强烈一致性对于所有偏航未对准值是一致的。然而,随着绝对偏航偏差的增加,BEM结果与SOWFA结果的偏差明显更大。OLAF和BEM结果之间的差异主要由偏航偏转角决定,不同的剪切指数和湍流强度会导致更细微的差异。总体而言,在具有挑战性的流入条件下,与SOWFA结果相比,OLAF结果比BEM结果更一致。
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引用次数: 1
Addressing deep array effects and impacts to wake steering with the cumulative-curl wake model 利用累积卷曲尾流模型解决深阵列效应和对尾流操纵的影响
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-03-24 DOI: 10.5194/wes-8-401-2023
C. Bay, P. Fleming, B. Doekemeijer, J. King, M. Churchfield, Rafael Mudafort
Abstract. Wind farm design and analysis heavily rely on computationally efficient engineering models that are evaluated many times to find an optimal solution. A recent article compared the state-of-the-art Gauss-curl hybrid (GCH) model to historical data of three offshore wind farms. Two points of model discrepancy were identified therein: poor wake predictions for turbines experiencing a lot of wakes and wake interactions between two turbines over long distances. The present article addresses those two concerns and presents the cumulative-curl (CC) model. Comparison of the CC model to high-fidelity simulation data and historical data of three offshore wind farms confirms the improved accuracy of the CC model over the GCH model in situations with large wake losses and wake recovery over large inter-turbine distances. Additionally, the CC model performs comparably to the GCH model for single- and fewer-turbine wake interactions, which were already accurately modeled. Lastly, the CC model has been implemented in a vectorized form, greatly reducing the computation time for many wind conditions. The CC model now enables reliable simulation studies for both small and large offshore wind farms at a low computational cost, thereby making it an ideal candidate for wake-steering optimization and layout optimization.
摘要风力发电场的设计和分析在很大程度上依赖于计算效率高的工程模型,这些模型需要多次评估才能找到最佳解决方案。最近的一篇文章将最先进的高斯-旋度混合(GCH)模型与三个海上风电场的历史数据进行了比较。其中确定了两个模型差异点:经历大量尾迹的涡轮机的尾迹预测差以及两个涡轮机之间长距离的尾迹相互作用。本文解决了这两个问题,并提出了累积旋度(CC)模型。将CC模型与三个海上风电场的高保真仿真数据和历史数据进行比较,证实了CC模型在较大机间距离的大尾迹损失和尾迹恢复情况下比GCH模型的精度有所提高。此外,CC模型在单涡轮和少涡轮尾迹相互作用方面的表现与GCH模型相当,这已经被精确地建模了。最后,将CC模型以矢量化的形式实现,大大减少了许多风况的计算时间。CC模型现在能够以较低的计算成本对小型和大型海上风电场进行可靠的模拟研究,从而使其成为尾流转向优化和布局优化的理想候选者。
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引用次数: 12
Actuator line model using simplified force calculation methods 采用简化力计算方法的执行器线模型
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-03-22 DOI: 10.5194/wes-8-363-2023
Gonzalo P. Navarro Diaz, A. Otero, H. Asmuth, Jens Nørkær Sørensen, S. Ivanell
Abstract. To simulate transient wind turbine wake interaction problems using limited wind turbine data, two new variants of the actuator line technique are proposed in which the rotor blade forces are computed locally using generic load data. The proposed models, which are extensions of the actuator disk force models proposed by Navarro Diaz et al. (2019a) and Sørensen et al. (2020), only demand thrust and power coefficients and the tip speed ratio as input parameters. In the paper the analogy between the actuator disk model (ADM) and the actuator line model (ALM)is shown, and from this a simple methodology to implement local forces in the ALM without the need for knowledge of blade geometry and local airfoil data is derived. Two simplified variants of ALMs are proposed, an analytical one based on Sørensen et al. (2020) and a numerical one based on Navarro Diaz et al. (2019a). The proposed models are compared to the ADM using analogous data, as well as to the classical ALM based on blade element theory, which provides more detailed force distributions by using airfoil data. To evaluate the local force calculation, the analysis of a partial-wake interaction case between two wind turbines is carried out for a uniform laminar inflow and for a turbulent neutral atmospheric boundary layer inflow. The computations are performed using the large eddy simulation facility in Open Source Field Operation and Manipulation (OpenFOAM), including Simulator for Wind Farm Applications (SOWFA)libraries and the reference National Renewable Energy Laboratory (NREL) 5 MW wind turbine as the test case. In the single-turbine case, computed normal and tangential force distributions along the blade showed a very good agreement between the employed models. The two new ALMs exhibited the same distribution as the ALM based on geometry and airfoil data, with minor differences due to the particular tip correction needed in the ALM.For the challenging partially impacted wake case, both the analytical and the numerical approaches manage to correctly capture the force distribution at the different regions of the rotor area, with, however, a consistent overestimation of the normal force outside the wake and an underestimation inside the wake. The analytical approach shows a slightly better performance in wake impact cases compared to the numerical one. As expected, the ALMs gave a much more detailed prediction of the higher-frequency power output fluctuations than the ADM. These promising findings open the possibility to simulate commercial wind farms in transient inflows using the ALM without having to get access to actual wind turbine and airfoil data, which in most cases are restricted due to confidentiality.
摘要为了使用有限的风力涡轮机数据模拟瞬态风力涡轮机尾流相互作用问题,提出了两种新的致动器线技术变体,其中使用通用载荷数据局部计算转子叶片力。所提出的模型是Navarro Diaz等人提出的致动器盘力模型的扩展。(2019a)和Sørensen等人。(2020),仅要求推力和功率系数以及叶尖速比作为输入参数。本文展示了致动器盘模型(ADM)和致动器线模型(ALM)之间的相似性,并由此导出了一种在ALM中实现局部力的简单方法,而无需了解叶片几何形状和局部翼型数据。提出了ALM的两个简化变体,一个是基于Sørensen等人的分析变体。(2020)和基于Navarro Diaz等人。(2019a)。将所提出的模型与使用类似数据的ADM以及基于叶片单元理论的经典ALM进行了比较,后者通过使用翼型数据提供了更详细的力分布。为了评估局部力计算,对均匀层流流入和湍流中性大气边界层流入的两台风力涡轮机之间的部分尾流相互作用情况进行了分析。计算是使用开源现场操作和操纵(OpenFOAM)中的大涡模拟设施进行的,包括风电场应用模拟器(SOWFA)库和参考国家可再生能源实验室(NREL)5 MW风机作为测试案例。在单涡轮机的情况下,沿叶片计算的法向力和切向力分布显示,所使用的模型之间非常一致。根据几何形状和翼型数据,两种新的ALM表现出与ALM相同的分布,但由于ALM中需要的特定叶尖校正,差异较小。对于具有挑战性的部分受冲击尾流情况,分析和数值方法都能正确捕捉转子区域不同区域的力分布,然而,尾流外法向力的一贯高估和尾流内的低估。与数值方法相比,分析方法在尾流碰撞情况下表现出略好的性能。正如预期的那样,ALM对更高频率的功率输出波动做出了比ADM更详细的预测。这些有希望的发现为使用ALM模拟瞬态流入的商业风电场提供了可能性,而无需访问实际的风力涡轮机和翼型数据,在大多数情况下,这些数据由于保密性而受到限制。
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引用次数: 3
Numerical simulations of ice accretion on wind turbine blades: are performance losses due to ice shape or surface roughness? 风力涡轮机叶片上结冰的数值模拟:性能损失是由于冰的形状还是表面粗糙度造成的?
IF 4 Q3 GREEN & SUSTAINABLE SCIENCE & TECHNOLOGY Pub Date : 2023-03-15 DOI: 10.5194/wes-8-341-2023
Francesco Caccia, A. Guardone
Abstract. Ice accretion on wind turbine blades causes both a change in the shape of its sections and an increase in surface roughness. These lead to degraded aerodynamic performances and lower power output. Here, a high-fidelity multi-step method is presented and applied to simulate a 3 h rime icing event on the National Renewable Energy Laboratory 5 MW wind turbine blade. Five sections belonging to the outer half of the blade were considered. Independent time steps were applied to each blade section to obtain detailed ice shapes. The roughness effect on airfoil performance was included in computational fluid dynamics simulations using an equivalent sand-grain approach. The aerodynamic coefficients of the iced sections were computed considering two different roughness heights and extensions along the blade surface. The power curve before and after the icing event was computed according to the Design Load Case 1.1 of the International Electrotechnical Commission. In the icing event under analysis, the decrease in power output strongly depended on wind speed and, in fact, tip speed ratio. Regarding the different roughness heights and extensions along the blade, power losses were qualitatively similar but significantly different in magnitude despite the well-developed ice shapes. It was found that extended roughness regions in the chordwise direction of the blade can become as detrimental as the ice shape itself.
摘要风力涡轮机叶片上的积冰导致其截面形状的变化和表面粗糙度的增加。这些导致空气动力学性能下降和功率输出降低。本文提出了一种高保真度的多步骤方法,并将其应用于3 国家可再生能源实验室的雾霾结冰事件5 MW风力涡轮机叶片。考虑了属于叶片外半部的五个部分。将独立的时间步长应用于每个叶片部分,以获得详细的冰形状。粗糙度对翼型性能的影响包括在使用等效沙粒方法的计算流体动力学模拟中。考虑到两种不同的粗糙度高度和沿叶片表面的延伸,计算了结冰截面的空气动力学系数。结冰事件前后的功率曲线是根据国际电工委员会的设计负载情况1.1计算的。在所分析的结冰事件中,功率输出的下降在很大程度上取决于风速,事实上,还取决于叶尖速比。关于不同的粗糙度高度和沿叶片的延伸,尽管冰的形状很发达,但功率损失在性质上相似,但在大小上明显不同。研究发现,叶片弦向上延伸的粗糙度区域可能与冰的形状本身一样有害。
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引用次数: 6
期刊
Wind Energy Science
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