کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
292806 | 511074 | 2016 | 12 صفحه PDF | دانلود رایگان |
• A wind tunnel test case of a complex double flutter instability in a long span bridge is presented.
• A multi-modal framework and a complete set of aerodynamic coefficients are necessary to simulate the phenomenon.
• The combination of several structural modes and sets of aerodynamic coefficients is studied.
An experimental double multi-modal flutter instability was recorded during wind tunnel tests on a full bridge aero elastic model. The analysis of this instability is presented in this paper, and it is studied with a multi-modal eigenvalue approach.It is shown that two different coupling mechanisms, one involving the symmetric modes and the other involving the anti-symmetric modes, lead to two different instabilities that occur at the same wind speed.The numerical analysis shows that a multi-modal framework and a complete set of aerodynamic coefficients are necessary to correctly estimate the flutter onset. The effect on flutter of structural and aerodynamic characteristics is discussed thoroughly, with a focus on structural modes and on the dependence of the aerodynamic coefficients upon the reduced velocity and upon the angle of attack.
Journal: Journal of Wind Engineering and Industrial Aerodynamics - Volume 151, April 2016, Pages 25–36