Computational Fluid Dynamics Approach to Aeroelastic Stability in Cable-Stayed Bridges
Long-span cable-supported bridges, such as cable-stayed and suspension bridges, are highly sensitive to wind-induced effects due to their flexibility, low damping, and relatively light weight. Aerodynamic analysis is therefore essential in their design and safety assessment. This study examines the aeroelastic stability of the Oued Dib cable-stayed bridge in Mila, Algeria, with emphasis on vortex shedding, galloping, torsional divergence, and classical flutter. A finite element modal analysis was carried out on a three-dimensional model to identify natural frequencies and mode shapes. A two-dimensional deck section was then analyzed using Computational Fluid Dynamics (CFD) under a steady wind flow of U = 20 m/s and varying angles of attack (AoA) from −10° to +10°. The simulations employed a RANS k-ω SST turbulence model with a wall function of Y+ = 30. The results provided detailed airflow patterns around the deck and enabled the evaluation of static aerodynamic coefficients—drag (CD), lift (CL), and moment (CM)—as functions of AoA. Finally, the bridge’s aeroelastic performance was assessed against the four instabilities. The findings indicate that the Oued Dib Bridge remains stable under the design wind conditions, although fatigue due to vortex shedding requires further consideration.
Authors
- Ehsan Harirchian (ORCID: https://orcid.org/0000-0003-0113-2120)
- Zouaoui Rabie Harrat (ORCID: https://orcid.org/0000-0001-9364-0506)
- Nadji Chioukh
- Zouhir S. M. Louhibi
- Sidi Mohammed Daoud (ORCID: https://orcid.org/0009-0007-5946-9152)
- Walid Mansour (ORCID: https://orcid.org/0000-0003-0955-6753)
Institutions
- Kafrelsheikh University (EG)
- Shenzhen University (CN)
- Université Djilali de Sidi Bel Abbès (DZ)
- Bauhaus-Universität Weimar (DE)
Publication Details
- Journal
- Buildings
- Published
- 2025-09-28
- DOI
- https://doi.org/10.3390/buildings15193509
- Primary Topic
- Fluid Dynamics and Vibration Analysis
- Type
- article
- Field-Weighted Citation Impact
- 0.00