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Analysis of self-excited forces for a box-girder bridge deck through unsteady RANS simulations
Affiliation:1. CRIACIV/Department of Civil and Environmental Engineering, University of Florence, Via S. Marta 3, 50139 Florence, Italy;2. Department of Civil and Environmental Engineering, University of Florence, Via S. Marta 3, 50139 Florence, Italy;3. Institute of Aeroelasticity, German Aerospace Center (DLR), Bunsenstraße 10, 37073 Göttingen, Germany;1. Department of Mechanical Engineering, Technical University of Denmark, Building 403, DK-2800 Kgs. Lyngby, Denmark;2. COWI Consulting Engineers and Planners A/S, Denmark;3. Computational Science and Engineering Laboratory, ETH Zürich, Clausiusstrasse 33, CH-8092 Zürich, Switzerland;1. School of Civil Engineering, University of A Coruña, Spain;2. Faculty of Engineering, University of Nottingham, UK;1. Key Laboratory of C & PC Structure of Ministry of Education, Southeast University, Nanjing 210096, China;2. College of Civil Engineering, Tongji University, Shanghai 200092, China;3. Wind Engineering Research Center, Hunan University, Changsha 410082, China;4. NatHaz Modeling Laboratory, University of Notre Dame, Notre Dame, IN 46556, USA
Abstract:This paper presents the results of two-dimensional numerical simulations of the flow field around a trapezoidal box-girder bridge section with later cantilevers, experiencing small-amplitude heaving or pitching harmonic oscillations. Unsteady Reynolds-averaged Navier–Stokes equations are solved in conjunction with an eddy-viscosity and an explicit algebraic Reynolds stress model. Flutter derivatives are determined and compared with wind tunnel results, showing fairly good agreement. The degree of sharpness of the deck lower edges is found to play a key role in the aeroelastic behavior of the profile. In particular, the bridge section fully behaves as a bluff body and is prone to low-reduced-wind-speed torsional galloping in the case of perfectly sharp edges. By contrast, the presence of a small radius of curvature in the section lower corners changes the nature of the instability to coupled flutter and significantly postpones the stability threshold, in line with a quasi-streamlined body behavior. Moreover, a wide sensitivity study is carried out, investigating the influence on the self-excited forces of the amplitude of oscillation, mean angle of attack and Reynolds number. In particular, the numerical simulations for the geometry with smooth lower edges highlight the regime transition occurring when the Reynolds number is varied, with significant effects on the flutter derivatives. Finally, the numerical flow visualizations provide a physical explanation of some phenomena observed in the wind tunnel experiments.
Keywords:Bridges aerodynamics  Self-excited forces  Flutter derivatives  Computational fluid dynamics  URANS  Reynolds number
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