...
首页> 外文期刊>Renewable energy >An experimental study on the aerodynamic performance degradation of a wind turbine blade model induced by ice accretion process
【24h】

An experimental study on the aerodynamic performance degradation of a wind turbine blade model induced by ice accretion process

机译:积冰过程引起的风力涡轮机叶片模型气动性能退化的实验研究

获取原文
获取原文并翻译 | 示例
           

摘要

An experimental study was conducted to characterize aerodynamic performance degradation of wind turbine blades induced by dynamic ice accretion process. The experimental study was performed in an Icing Research Tunnel with a turbine blade model under a typical glaze icing condition. Ice structures were found to accrete rapidly over both the upper and lower surfaces of the blade model after starting the ice accretion experiment. Irregular-shaped ice structures were found to disturb the airflow around the blade model greatly, resulting in large-scale flow separations and shedding of unsteady vortex structures from the ice accreting surface. The aerodynamic performance of the blade model was found to degrade significantly. The performance degradation induced by the ice accretion was found to be a strong function of the angle of attack of the blade model with more significant degradations at lower angles of attack. For the test case at the angle of attack of 5.0, while the lift decreases to only-12% of its original value after 600 s of the ice accretion experiment, the drag was found to increase 4.5 times correspondingly. The detailed flow field measurements were correlated with the aerodynamic force data to elucidate the underlying physics. (C) 2018 Elsevier Ltd. All rights reserved.
机译:进行了一项实验研究,以表征由动态积冰过程引起的风力涡轮机叶片的空气动力性能下降。在典型的釉面结冰条件下,在具有涡轮叶片模型的结冰研究隧道中进行了实验研究。在开始积冰实验后,发现冰结构在叶片模型的上表面和下表面均迅速积聚。发现不规则形状的冰结构极大地干扰了叶片模型周围的气流,从而导致大规模的流动分离和不稳定的涡旋结构从积冰表面脱落。发现叶片模型的空气动力学性能显着降低。发现由积冰引起的性能下降是叶片模型的迎角的强函数,而在较低的迎角下则表现出更大的退化。对于攻角为5.0的测试案例,在吸冰实验600 s之后,升力降低到其原始值的-12%,而阻力却相应地增加了4.5倍。详细的流场测量结果与空气动力学力数据相关联,以阐明基本物理原理。 (C)2018 Elsevier Ltd.保留所有权利。

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