Efficient numerical investigation of flow control on wind turbine rotors under realistic conditions

实际条件下风力涡轮机转子流动控制的高效数值研究

基本信息

项目摘要

The common goal of the research focus is the improvement of design and calculation methods for wind turbine load control solutions through experimental and numerical means. In addition to detailed high fidelity CFD simulations, engineering level design tools, which allow for parametric investigations or certification like simulations of different flow control concepts were developed during the first project phase. Additionally these tools are also used to project experimentally obtained results from wind tunnel tests to real size wind turbines. In PP1, a toolchain for the aero-elastic and unsteady simulation of flow control equipped wind turbine rotors has been established and validated. Successively the performance and feasibility of different flow control technologies considering realistic inflow conditions and aero elastic effects was investigated. However, many additional aspects of load control applications need further investigation before this technology can be integrated in the complex wind turbine system. To realistically asses the performance and potential of active and passive flow control, advanced simulations that not only include realistic unsteady aerodynamics, inflow and structural, but also realistic wind turbine controllers, shall be carried out. As wind turbines are often clustered in large windfarms, the effects of wake-rotor interactions on flow control performance, and the effect of flow control solutions on the loads and yield of successive turbines are questions that will also be addressed within the proposed prolongation. To achieve such feasibility for the simulation tools the functionality will be extended around the following aspects: In a first step the aerodynamic model will be extended with an advanced dynamic stall model, which also captures the dynamic lift response of flap movement. To enable the investigation of the interaction between flow control elements, their control and the resulting load changes with the main wind turbine controller, wind turbine controllers will be integrated in the simulation environment. Furthermore the code will be extended such that the mutual interaction between wind turbines in a wind park and the effects of this wake-turbine interaction on the feasibility and performance of different load control systems can be simulated. A focus during the continuation of development will be set on computational efficiency, as it is necessary to simulate a large amount of load cases to fully address the feasibility and performance of load control on wind turbine rotors.
研究的共同目标是通过实验和数值手段改进风力涡轮机负载控制解决方案的设计和计算方法。除了详细的高保真CFD模拟外,在第一个项目阶段还开发了工程级设计工具,这些工具允许进行参数调查或认证,如不同流量控制概念的模拟。此外,这些工具还用于将从风洞试验获得的实验结果投影到真实的尺寸的风力涡轮机。在PP 1中,已经建立并验证了用于装有流控的风力涡轮机转子的气动弹性和非定常模拟的工具链。随后,考虑实际来流条件和气动弹性效应,研究了不同流动控制技术的性能和可行性。然而,在将该技术集成到复杂的风力涡轮机系统中之前,需要进一步研究负载控制应用的许多其他方面。为了真实地评估主动和被动流量控制的性能和潜力,应进行高级模拟,不仅包括真实的非定常空气动力学、流入和结构,还包括真实的风力涡轮机控制器。由于风力涡轮机通常集中在大型风电场中,尾流-转子相互作用对流量控制性能的影响,以及流量控制解决方案对连续涡轮机的负载和产量的影响,也将在拟议的延长期内解决。为了实现这种可行性的仿真工具的功能将围绕以下几个方面进行扩展:在第一步,空气动力学模型将扩展为先进的动态失速模型,该模型还可以捕获襟翼运动的动态升力响应。为了能够研究流量控制元件之间的相互作用、它们的控制以及主风力涡轮机控制器导致的负载变化,风力涡轮机控制器将被集成到仿真环境中。此外,该代码将被扩展,使得风力发电场中的风力涡轮机之间的相互作用以及这种尾流-涡轮机相互作用对不同负载控制系统的可行性和性能的影响可以被模拟。在继续开发过程中,重点将放在计算效率上,因为有必要模拟大量的负载情况,以充分解决风力涡轮机转子负载控制的可行性和性能。

项目成果

期刊论文数量(10)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
Coupling of an Unsteady Lifting Line Free Vortex Wake Code to the Aeroelastic HAWT Simulation Suite FAST
  • DOI:
    10.1115/gt2016-56290
  • 发表时间:
    2016-09
  • 期刊:
  • 影响因子:
    0
  • 作者:
    J. Saverin;D. Marten;G. Pechlivanoglou;C. Nayeri;C. Paschereit
  • 通讯作者:
    J. Saverin;D. Marten;G. Pechlivanoglou;C. Nayeri;C. Paschereit
Implementation of the Multi-Level Multi-Integration Cluster Method to the Treatment of Vortex Particle Interactions for Fast Wind Turbine Wake Simulations
多级多积分聚类方法的实现,用于处理快速风力涡轮机尾流模拟中的涡粒子相互作用
Advanced Medium-Order Modelling of a Wind Turbine Wake with a Vortex Particle Method Integrated within a Multilevel Code
使用集成在多级代码中的涡粒子方法对风力涡轮机尾流进行高级中阶建模
  • DOI:
    10.1088/1742-6596/1037/6/062029
  • 发表时间:
    2018
  • 期刊:
  • 影响因子:
    0
  • 作者:
    Saverin;Marten;Pechlivanoglou;Oliver Paschereit
  • 通讯作者:
    Oliver Paschereit
Aeroelastic simulation of multi-MW wind turbines using a free vortex model coupled to a geometrically exact beam model
  • DOI:
    10.1088/1742-6596/753/8/082015
  • 发表时间:
    2016-09
  • 期刊:
  • 影响因子:
    0
  • 作者:
    J. Saverin;J. Peukert;D. Marten;G. Pechlivanoglou;C. Paschereit;D. Greenblatt
  • 通讯作者:
    J. Saverin;J. Peukert;D. Marten;G. Pechlivanoglou;C. Paschereit;D. Greenblatt
Numerical and Experimental Investigation of Trailing Edge Flap Performance on a Model Wind Turbine
模型风力涡轮机后缘襟翼性能的数值和实验研究
  • DOI:
    10.2514/6.2018-1246
  • 发表时间:
    2018
  • 期刊:
  • 影响因子:
    0
  • 作者:
    Marten;Bartholomay;Pechlivanoglou;Nayeri;Paschereit;Fischer
  • 通讯作者:
    Fischer
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Professor Dr.-Ing. Christian Oliver Paschereit其他文献

Professor Dr.-Ing. Christian Oliver Paschereit的其他文献

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{{ truncateString('Professor Dr.-Ing. Christian Oliver Paschereit', 18)}}的其他基金

The Interaction between a Spatially Oscillating Jet and a Crossflow
空间振荡射流与横流之间的相互作用
  • 批准号:
    289230680
  • 财政年份:
    2016
  • 资助金额:
    --
  • 项目类别:
    Research Grants
Experimental investigation of the impact of temperature stratification on the occurrence of a global mode in swirling jets undergoing vortex breakdown
温度分层对旋涡射流涡流破裂中全局模态发生影响的实验研究
  • 批准号:
    250934256
  • 财政年份:
    2014
  • 资助金额:
    --
  • 项目类别:
    Research Grants
Active Micro-Tabs for Load Control on Wind Turbine Blades
用于风力涡轮机叶片负载控制的主动微型片
  • 批准号:
    236580630
  • 财政年份:
    2013
  • 资助金额:
    --
  • 项目类别:
    Research Grants
Investigation of the Unsteady Wake behind a Generic Tractor-Trailer with Different Boundary Conditions
不同边界条件下通用牵引挂车后非定常尾流的研究
  • 批准号:
    235211755
  • 财政年份:
    2013
  • 资助金额:
    --
  • 项目类别:
    Research Grants
Development of active flow control methods utilizing steady and pulsed plasma actuators for low speed flight Reynolds numbers
利用稳定和脉冲等离子体致动器开发用于低速飞行雷诺数的主动流量控制方法
  • 批准号:
    209952577
  • 财政年份:
    2012
  • 资助金额:
    --
  • 项目类别:
    Research Grants
Experimentelle Untersuchung der Schallabstrahlung einer turbulenten vorgemischten Freistrahlflamme
湍流预混自由射流火焰声辐射的实验研究
  • 批准号:
    135599953
  • 财政年份:
    2010
  • 资助金额:
    --
  • 项目类别:
    Research Grants
Response of generic swirl flames to transverse acoustic forcing
一般旋涡火焰对横向声强迫的响应
  • 批准号:
    175585448
  • 财政年份:
    2010
  • 资助金额:
    --
  • 项目类别:
    Research Grants
Akustische Nahfeldholographie in Brennkammern, Methodenentwicklung und experimentelle Umsetzung
燃烧室中的声近场全息术、方法开发和实验实施
  • 批准号:
    151186185
  • 财政年份:
    2009
  • 资助金额:
    --
  • 项目类别:
    Research Grants
Numerische Berechnung der Schadstoffbildung einer mager technisch vorgemischten, turbulenten Flamme mit LEM als Subgrid-Modell für LES.
使用 LEM 作为 LES 的子网格模型,对稀薄、技术上预混合的湍流火焰的污染物形成进行数值计算。
  • 批准号:
    53408007
  • 财政年份:
    2008
  • 资助金额:
    --
  • 项目类别:
    Research Grants
Open- and closed-loop control of instabilities in swirling jets undergoing vortex breakdown with application to swirl-stabilized burner flows
对经历涡流破坏的旋流射流不稳定性的开环和闭环控制及其在旋流稳定燃烧器流中的应用
  • 批准号:
    70100893
  • 财政年份:
    2008
  • 资助金额:
    --
  • 项目类别:
    Research Grants

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超声行波微流体驱动机理的试验研究
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