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contributor authorF. Y. Xu
date accessioned2017-05-08T22:20:52Z
date available2017-05-08T22:20:52Z
date copyrightMay 2015
date issued2015
identifier other42676547.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/78329
description abstractThe extraction of 18 flutter derivatives of bridge decks from three degree-of-freedom (3-DOF) free vibration data using a novel direct approach is addressed in this study. Different with many conventional methods that construct a system state matrix, this approach directly extracts 18 flutter derivatives using the aeroelastically modified modal parameters. No state matrix is concerned, and thus it is more straightforward from the physical essence viewpoint. The validity and accuracy are demonstrated by a 3-DOF numerical example for bridge deck model. Afterward, the 18 flutter derivatives of two exact bridge decks with representative streamlined and bluff sections are extracted. Detailed deterministic and stochastic vulnerability analyses on identification accuracy of modal parameters and flutter derivatives were conducted for the numerical model and two bridge decks. For the free vibration method, the potential uncertainties in aeroelastic parameter determination are investigated, and the causes of low accuracy of some flutter derivatives (e.g.,
publisherAmerican Society of Civil Engineers
titleDirect Approach to Extracting 18 Flutter Derivatives of Bridge Decks and Vulnerability Analysis on Identification Accuracy
typeJournal Paper
journal volume28
journal issue3
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000413
treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 003
contenttypeFulltext


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