ON THE FLUTTER INSTABILITY OF A SUSPENSION BRIDGE USING THE FINITE ELEMENT METHOD
The study of aeroelastic instability is fundamental for the feasibility of a large span suspension bridge. The determination of the flutter wind velocity is generally determined by a two-degrees-of-freedom model. In this paper an analytical model is developed to predict the flutter behavior of a suspension bridge, with a multi-degrees-of-freedom system. A finite element technique is employed. The numerical difficulties related to the solution of the problem are discussed. A suitable method is developed to increase the numerical stability of the solution. As an example, the results of the method are applied to the Messina crossing project.
- Prepared for meeting held September 26-30, 1977.
American Society of Mechanical EngineersTwo Park Avenue
New York, NY United States 10016-5990
- DIANA, G
- Falco, M
- Gasparetto, M
- Publication Date: 1977-9
- Features: References;
- Pagination: 11 p.
- TRT Terms: Aerodynamic force; Aerodynamics; Bridges; Chemical processes; Deformation; Dynamic loads; Finite element method; Flutter (Aeronautics); Flutter (Aeronautics); Forecasting; Mathematical methods; Mathematical models; Stability (Mechanics); Stability analysis; Structural analysis; Suspension bridges; Velocity; Wind
- Uncontrolled Terms: Dynamic response
- Old TRIS Terms: Aerobic processes; Wind effects; Wind velocity
- Subject Areas: Bridges and other structures; Highways;
- Accession Number: 00173561
- Record Type: Publication
- Source Agency: Engineering Index
- Report/Paper Numbers: ASME 77-DET-150
- Files: TRIS
- Created Date: Jun 28 1978 12:00AM