首页> 外文OA文献 >Wind tunnel tests of a free yawing downwind wind turbine
【2h】

Wind tunnel tests of a free yawing downwind wind turbine

机译:自由偏航顺风风力涡轮机的风洞试验

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。

摘要

During February and April 2012 a series of wind tunnel tests were performed at the TU Delft Open Jet Facility (OJF) with a three bladed downwind wind turbine and a rotor radius of 0.8 meters. The setup includes an off the shelf three bladed hub, nacelle and generator on which relatively flexible blades are mounted. The tower support structure has free yawing capabilities provided at the tower base. A short overview on the technical details of the experiment is provided as well as a brief summary of the design process. The discussed test cases show that the turbine is stable while operating in free yawingconditions. Further, the effect of the tower shadow passage on the blade flapwise strain measurement is evaluated. Finally, data from the experiment is compared with preliminary simulations using DTU Wind Energy's aeroelastic simulation program HAWC2.
机译:在2012年2月和2012年4月期间,在TU代尔夫特露天喷气式飞机场(OJF)进行了一系列风洞测试,其中装有三叶顺风风力涡轮机,转子半径为0.8米。该装置包括一个现成的三叶轮毂,机舱和发电机,其上安装了相对灵活的叶片。塔架支撑结构具有在塔架基座处提供的自由偏航功能。提供了有关实验技术细节的简短概述以及设计过程的简短摘要。讨论的测试案例表明,在自由偏航条件下运行时,涡轮机是稳定的。此外,评估了塔影通道对叶片翼向应变测量的影响。最后,将实验数据与使用DTU Wind Energy的气动弹性仿真程序HAWC2进行的初步仿真进行比较。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
代理获取

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号