Experimental investigation of combined vibrations for a hydrofoil-rod system at low Reynold numbers

被引:0
作者
Ren-feng Wang
Ke Chen
Francis Nobelesse
Yun-xiang You
Wei Li
机构
[1] Shanghai Jiao Tong University,State Key Laboratory of Ocean Engineering
[2] Collaborative Innovation Center for Advanced Ship and Deep-Sea Exploration,undefined
来源
Journal of Hydrodynamics | 2019年 / 31卷
关键词
Vibrations; lifting bodies; transition; laminar separation bubbles;
D O I
暂无
中图分类号
学科分类号
摘要
A hydrodynamic tunnel experimental investigation and analysis of vibration characteristics for a hydrofoil in a transient regime is considered. Tests are performed for NACA 0017 models with a non-uniform section at an angle of attack AOA = 5º and Reynolds numbers up to Re = 7.0 × 106. This study is related to a project design of experiments in a complex facility that involves several parameters. The analysis focuses on the vibrations of a hydrofoil for different values of the bracing stiffness kh, the torsional stiffness ka, and the locations of the elastic axis ā and of the center of gravity xa. The structural bracing response is investigated via measurements of the displacement of the free tip section of the hydrofoil using a three-axis acceleration sensor, and the torsional response of the structure is analyzed via measurements of displacements with single-axis acceleration sensors. The hydrofoil is made of reinforced plastics without flexibility, and elastic functions are provided by a spring support mechanism combined with a torsional structure. The study shows that an increase of the velocity V∞ results in different behaviors of the bracing and torsional amplitudes. Another notable result of the study is that the emergence of transition occurs simultaneously with additional peaks and changes of vibration amplitudes.
引用
收藏
页码:512 / 521
页数:9
相关论文
共 24 条
[1]  
Rojratsirikul P.(2011)Flow–induced vibrations of low aspect ratio rectangular membrane wings [J] Journal of Fluids and Structures 27 1296-1309
[2]  
Genc M. S.(2003)Membrane wing aerodynamics for micro air vehicles [J] Progress in Aerospace Sciences 39 425-465
[3]  
Wang Z.(2007)Laminar–turbulent transition of a low reynolds number rigid or flexible airfoil [J] AIAA journal 45 1501-1513
[4]  
Lian Y.(2008)An experimental study of the laminar flow separation on a low–reynolds–number airfoil [J] Journal of Fluids Engineering 130 051101-509
[5]  
Shyy W.(2002)Investigations of time–growing instabilities in laminar separation bubbles [J] European Journal of Mechanics–B/Fluids 21 495-1485
[6]  
Viieru D.(2013)Transient loads occurring over a thin airfoil subjected to large–scale freestream turbulence [J] AIAA Journal 51 1473-17
[7]  
Lian Y.(2015)Dynamic pitching effect on a laminar separation bubble [J] Experiments in Fluids 56 1-2279
[8]  
Shyy W.(2015)Control of laminar separation bubble on naca 0009 airfoil using electroactive polymers [J] AIAA Journal 53 2270-51
[9]  
Hu H.(2012)An experimental study of boundary–layer transition induced vibrations on a hydrofoil [J] Journal of Fluids and Structures 32 37-undefined
[10]  
Yang Z.(undefined)undefined undefined undefined undefined-undefined