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Compliant flow designs for optimum lift control of wind turbine rotors.

机译:顺应流量设计,可实现风力涡轮机转子的最佳升程控制。

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摘要

An optimization approach was formulated to determine geometric designs that are most compliant to flow control devices. Single dielectric barrier discharge (SDBD) plasma actuators are used in the flow control design optimization as they are able to be incorporated into CFD simulations. An adjoint formulation was derived in order to have a numerically efficient way of calculating the shape derivatives on the surface of the geometric design.;The design of a wind turbine blade retrofit for the JIMP 25kW wind turbine at Notre Dame is used to motivate analyses that utilize the optimization approach. The CFD simulations of the existing wind turbine blade were validated against wind tunnel testing.;A one-parameter optimization was performed in order to design a trailing edge addition for the current wind turbine blade. The trailing edge addition was designed to meet a desired lift target while maximizing the lift-to-drag ratio. This analysis was performed at seven radial locations on the wind turbine blade. The new trailing edge retrofits were able to achieve the lift target for the outboard radial locations. The designed geometry has been fabricated and is currently being validated on a full-scale turbine and it is predicted to have an increase in annual energy production of 4.30%.;The design of a trailing edge retrofit that includes the use of a SDBD plasma actuator was performed using a two-parameter optimization. The objective of this analysis was to meet the lift target and maximize the controllability of the design. The controllability is defined as the difference in lift between plasma on and plasma off cases. A trailing edge retrofit with the plasma actuator located on the pressure side was able to achieve the target passive lift increase while using plasma flow control to reduce the lift to below the original design. This design resulted in a highly compliant flow.
机译:制定了一种优化方法来确定最符合流量控制设备的几何设计。单电介质势垒放电(SDBD)等离子体致动器可用于流量控制设计优化,因为它们可以被纳入CFD模拟中。推导了一个伴随公式,以便采用有效的数值方法来计算几何设计表面上的形状导数。;巴黎圣母院JIMP 25kW风力涡轮机的风力涡轮机叶片改造设计用于激发分析工作,利用优化方法。通过风洞测试验证了现有风力涡轮机叶片的CFD模拟。;进行了一个参数优化,以设计当前风力涡轮机叶片的后缘。后缘附加件旨在满足所需的提升目标,同时最大程度地提高提升阻力比。该分析是在风力涡轮机叶片上的七个径向位置进行的。新的后缘改造能够实现外侧径向位置的提升目标。所设计的几何形状已经制造出来,目前正在全尺寸涡轮机上进行验证,并且预计将使年发电量增加4.30%。;后缘改造的设计包括使用SDBD等离子致动器使用两参数优化执行。该分析的目的是满足提升目标并最大程度地提高设计的可控制性。可控制性定义为等离子开启和等离子关闭情况之间的升程差。使用位于压力侧的等离子执行器进行后缘改造,可以实现目标被动升程的增加,同时使用等离子流控制将升程降低到原始设计以下。这种设计产生了高度合规的流程。

著录项

  • 作者

    Williams, Theodore J.H.;

  • 作者单位

    University of Notre Dame.;

  • 授予单位 University of Notre Dame.;
  • 学科 Engineering Aerospace.;Energy.
  • 学位 Ph.D.
  • 年度 2014
  • 页码 170 p.
  • 总页数 170
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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