Abstract
The work presents a 3D aeroelastic model of a long-span suspension bridge with streamlined deck equipped with leading- and trailing-edge flaps. The objective is to devise a model for the computation of the bridge stability (flutter and torsional divergence) and forced response (buffeting), yet of manageable size to allow for modern control design. The Humber Bridge (UK) is used as a design example. Both fully erected and partially erected conditions are considered. The comparison with previous published data and the results of a preliminary robust controller aimed at increasing the flutter critical velocity and reducing the buffeting are included.
Original language | English |
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Publication status | Published - 2015 |
Externally published | Yes |
Event | 16th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015 - Saint Petersburg, Russian Federation Duration: 28 Jun 2015 → 2 Jul 2015 |
Conference
Conference | 16th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015 |
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Country/Territory | Russian Federation |
City | Saint Petersburg |
Period | 28/06/15 → 2/07/15 |
Keywords
- Aeroelasticity
- Buffeting
- Control
- Flaps
- Flutter
- Long-span bridge
- Winglets
ASJC Scopus subject areas
- Mechanical Engineering
- Aerospace Engineering