首页> 外文会议>ASME joint US-European Fluids Engineering Division summer meeting >AN EXPERIMENTAL STUDY OF THE WIND-DRIVEN WATER DROPLET/RIVULET FLOWS OVER AN AIRFOIL PERTINENT TO WIND TURBINE ICING PHENOMENA
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AN EXPERIMENTAL STUDY OF THE WIND-DRIVEN WATER DROPLET/RIVULET FLOWS OVER AN AIRFOIL PERTINENT TO WIND TURBINE ICING PHENOMENA

机译:风轮结冰现象的翼型上方的风驱动水/水流流动的实验研究

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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:在寒冷的天气中,风力涡轮机的结冰是对风力涡轮机完整性的最大威胁。推进在大气结冰条件下安全,高效地运行风力涡轮机的技术要求开发针对缓解和保护风力涡轮机结冰而量身定制的创新,有效的除冰/除冰策略。这样做需要对与风力涡轮机结冰现象有关的复杂热流现象的基本物理知识有深刻的了解,既要为结冰本身,也要为沿着风力涡轮机叶片被污染表面的水倒流。在本研究中,进行了一项实验研究,以表征在NACA 0012机翼上流动的地表风驱动水膜/小流,以阐明与风力涡轮机结冰现象有关的瞬态地表水运输行为的基本物理原理。实验研究是在爱荷华州立大学航空工程系的结冰研究风洞中进行的。开发了一种新颖的数字图像投影(DIP)测量系统,并将其应用于在不同测试条件下对地表水膜/小溪流的厚度分布进行定量测量。测量结果清楚地表明,在撞击到NACA0012机翼的前缘之后,微小尺寸的水滴会聚结,在机翼前缘附近的区域中形成薄水膜。发现小溪的形成是时间依赖的过程,并且依赖于初始的水流径流结构。发现水铆钉的宽度和间距随着风速的增加而单调减小。膜厚结冰定律通过时间平均测量膜厚来评价。测量结果显示出与解析缩放预测相一致的良好结果。

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