尾缘柔性变形对翼型水动力学性能的影响
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  • 英文篇名:Influence of Trailing Edge Flexible Deformation on Hydrodynamic Performance of Hydrofoil
  • 作者:张敬斌 ; 王树杰 ; 袁鹏 ; 谭俊哲 ; 司先才
  • 英文作者:ZHANG Jing-Bin;WANG Shu-Jie;YUAN Peng;TAN Jun-Zhe;SI Xian-Cai;College of Engineering,Ocean University of China;Ocean Engineering Key Lab of Qingdao;
  • 关键词:潮流能水轮机 ; 柔性叶片 ; 尾缘柔性变形 ; 升阻力系数 ; 水动力学性能
  • 英文关键词:tidal turbine;;flexible blade;;trailing edge flexible deformation;;lift and drag coefficient;;hydrodynamic performance
  • 中文刊名:QDHY
  • 英文刊名:Periodical of Ocean University of China
  • 机构:中国海洋大学工程学院;青岛市海洋可再生能源重点实验室;
  • 出版日期:2018-11-23
  • 出版单位:中国海洋大学学报(自然科学版)
  • 年:2019
  • 期:v.49;No.290
  • 基金:国家自然科学基金项目(51479185);; 山东省重点研发计划项目(2015GSF115019)资助~~
  • 语种:中文;
  • 页:QDHY201901015
  • 页数:7
  • CN:01
  • ISSN:37-1414/P
  • 分类号:124-130
摘要
流体机械柔性叶片特有的性能引起越来越多的关注,柔性叶片潮流能水轮机因叶片自适应变形,具有不同于刚性叶片水轮机的水动力学性能。首先从二维层面分析柔性尾缘变形对翼型水动力学性能的影响。利用ANSYS对创建的柔性叶片模型进行静力学分析,获得翼型截面变形后的节点数据,建立变形后的翼型模型。利用CFD仿真软件,采用k-ωSST的湍流模型,对比分析原始翼型和变形后翼型升阻力系数、表面压力系数分布及流场变化。结果表明:尾缘柔性变形对翼型性能有较大影响,适当变形可以提高翼型的升力系数;变形后翼型升阻比在一定攻角下大于原始翼型,有利于改善原始翼型的水动力学性能。
        There is growing concern about the inherent performance of flexible blade of fluid machinery.The dynamic performance of the flexible blade tidal turbine is different from that of the rigid blade turbine due to adaptive deformation of the blades.Two dimensional analysis was conducted on the effect of flexible trailing edge bending of the hydrofoil on its hydrodynamic performance.Static analysis was carried out on the flexible blade model by using software ANSYS,data of the nods of the hydrofoil section was obtained,and the model of the hydrofoil after deformation was established.By using CFD simulation software with the k-ωSST turbulence model,lift and drag coefficient,surface pressure coefficient and flow field of the hydrofoil before and after deformation was compared.The results show that the flexible deformation of the trailing edge had a great influence on the performance of the hydrofoil,and the lift coefficient of the airfoil could be improved by right deformation;The hydrofoil lift drag ratio at a certain angle of attack was larger than that of the original hydrofoil,which helps to improve the hydrodynamic performance of the original hydrofoil.
引文
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