IDENTIFICATION OF AEROELASTIC PARAMETERS OF FLEXIBLE BRIDGES

Simultaneous extraction of all the aeroelastic parameters of a flexibl e bridge deck from a single section-model test has been a desirable go al not fully attained in the past. In the work reported herein, an exp erimental setup was designed for executing coupled vertical-torsional motion of a section model. In the present instance, the section model was located in proximity to a fixed model representing a section of th e adjacent deck of a twin-deck configuration. A robust system-identifi cation method was developed and applied to the noise-corrupted displac ement time histories of the section model. The experimental setup, the method of extracting the aeroelastic parameters, and the implications of the results obtained are presented in this paper. The tests were p erformed under both smooth and turbulent flow conditions, and in both the presence and absence of the second deck. This technique proved to offer good performance, which is evident from the consistent aeroelast ic parameters obtained.