location: Current position: Home >> Scientific Research >> Paper Publications

Free vibration numerical simulation technique for extracting flutter derivatives of bridge decks

Hits:

Indexed by:期刊论文

Date of Publication:2017-11-01

Journal:JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS

Included Journals:Scopus、SCIE、EI

Volume:170

Page Number:226-237

ISSN No.:0167-6105

Key Words:Flutter derivatives; Free vibration; Numerical simulation; Bridge aerodynamics

Abstract:A numerical simulation technique based on computational fluid dynamics (CFD) for determining the time-varying histories of free vibration displacements, velocities, and aerodynamic forces of bridge decks is presented. The weak coupling method is used to address the problem of fluid-structure-interaction (FSI). The flutter derivatives can be conveniently extracted using the numerically simulated displacements, velocities, and aerodynamic forces, which is similar to the procedure adopted in the forced vibration method. First, the identification accuracy of flutter derivatives is validated by comparison with the theoretical results for an ideal thin plate. Then, the flutter derivatives of two typical bridge deck sections, one streamlined and one bluff, are extracted by the proposed method. The results of the streamlined section show good agreement with other methods. However, for the bluff section, noticeable discrepancies exist between different methods. The mean angle of incidence in the free vibration method is shown to be responsible for these disagreements. The strengths of the newly-proposed approach are compared with those of the numerical and experimental forced vibration and experimental free vibration methods. This convenient and effective approach may serve as a building block for extracting flutter derivatives and better understanding of the aeroelastic responses of long-span flexible bridges.

Pre One:Three-Degree-of-Freedom Coupled Numerical Technique for Extracting Eighteen aerodynamic Derivatives of Bridge Decks

Next One:Spanwise length and mesh resolution effects on simulated fl ow around a 5:1 rectangular cylinder