首页> 外文会议>ASME Fluids Engineering Division Meeting >AN EXPERIMENTAL STUDY OF THE WIND-DRIVEN WATER DROPLET/RIVULET FLOWS OVER AN AIRFOIL PERTINENT TO WIND TURBINE ICING PHENOMENA
【24h】

AN EXPERIMENTAL STUDY OF THE WIND-DRIVEN WATER DROPLET/RIVULET FLOWS OVER AN AIRFOIL PERTINENT TO WIND TURBINE ICING PHENOMENA

机译:风力驱动的水滴/竖坯流过上有关风力涡轮机结冰现象的翼型流动的实验研究

获取原文

摘要

Wind turbine icing represents the most significant threat to the integrity of wind turbines in cold weather. Advancing the technology for safe and efficient wind turbine operation in atmospheric icing conditions requires the development of innovative, effective anti-/de-icing strategies tailored for wind turbine icing mitigation and protection. Doing so requires a keen understanding of the underlying physics of complicated thermal flow phenomena pertinent to wind turbine icing phenomena, both for the icing itself as well as for the water runback along contaminated surfaces of wind turbine blades. In the present study, an experimental investigation was conducted to characterize the surface wind-driven water film/rivulet flows over a NACA 0012 airfoil in order to elucidate the underlying physics of the transient surface water transport behavior pertinent to wind turbine icing phenomena. The experimental study was conducted in an icing research wind tunnel available at Aerospace Engineering Department of Iowa State University. A novel digital image projection (DIP) measurement system was developed and applied to achieve quantitative measurements of the thickness distributions of the surface water film/rivulet flow at different test conditions. The measurement results reveal clearly that, after impinged on the leading edge of the NACA0012 airfoil, the micro-sized water droplets would coalesce to form a thin water film in the region near the leading edge of the airfoil. The formation of rivulets was found to be time-dependent process and relies on the initial water runback flow structure. The width and the spacing of the water rivulets were found to decrease monotonically with the increasing wind speed. The film thickness icing scaling law is evaluated by the time-average measurement film thickness. The measurement results show good consistent with the analytical scaling predictions.
机译:风力涡轮机结冰代表了对寒冷天气中风力涡轮机完整性的最重要威胁。在大气锦冰条件下推进安全有效的风力涡轮机运行,需要开发创新,有效的抗糖浆策略,为风力涡轮机结冰缓解和保护。这样做需要对有关风力涡轮机结冰现象的复杂热流现象的潜在物理的敏锐理解,两者都是糖衣本身以及沿着风力涡轮机叶片的污染表面的水回路。在本研究中,进行实验研究以表征表面风力驱动的水膜/铆钉在NACA 0012翼型上流动,以便阐明与风力涡轮机结冰现象有关的瞬态表面水运输行为的底层物理。实验研究是在爱荷华州立大学航空航天工程系的冰开隧道中进行。开发并应用了一种新型数字图像投影(DIP)测量系统,以实现不同测试条件下表面水膜/ ripulet流的厚度分布的定量测量。测量结果清楚地揭示了在撞击NaCA0012翼型的前缘之后,微尺寸的水滴将在翼型的前缘附近形成薄的水膜。发现铆钉的形成是时间依赖的过程,并依赖于初始水回路流动结构。发现水流轴的宽度和间隔随着风速而单调地减小。通过时间平均测量膜厚度评估薄膜厚度结冰规律。测量结果显示出与分析缩放预测的符合。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

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