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dc.contributor.authorBrownjohn, James
dc.contributor.authorChoi, ECC
dc.date.accessioned2016-02-01T14:09:01Z
dc.date.issued2001-10
dc.description.abstractWind tunnel tests were conducted on a model of deck section from the Ting Kau cablernstayed bridge. The purpose of the tests was to determine the set of aerodynamic derivatives conventionallyrnused to describe the motion-induced forces arising from the wind flow, and to investigate the stability ofrnthe deck under different conditions of turbulence and angle of attack. The study shows that except forrnlarge negative angles of attack the deck section itself is stable up to a high wind speed, and that whenrninstability does occur it is essentially a single degree of freedom (torsional) flutter.en_GB
dc.identifier.citationVol. 4, No.5, pp. 367 - 382en_GB
dc.identifier.doi10.12989/was.2001.4.5.367
dc.identifier.urihttp://hdl.handle.net/10871/19479
dc.publisherWileyen_GB
dc.rights.embargoreasonUnder indefinite embargo – no publisher permission. The final version is available from the publisher via the DOI in this record.en_GB
dc.titleWind tunnel section model study of aeroelastic performance for Ting Kau Bridge Decken_GB
dc.typeArticleen_GB
dc.identifier.issn1226-6116
dc.identifier.journalWind and Structuresen_GB


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