2005
DOI: 10.1016/j.jsv.2004.01.026
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Buffeting response of long-span cable-supported bridges under skew winds. Part 1: theory

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Cited by 58 publications
(21 citation statements)
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“…These programs are now used to perform the structural internal force responses prediction of the Tsing Ma suspension Bridge with a main span of 1377m. The aerodynamic and aeroelastic parameters of bridge deck are taken from the wind tunnel test results (Zhu, 2002) and the reference mean wind speed is taken as 25m/s. The studied cases are listed in table 1.…”
Section: Random Vibration Methodsmentioning
confidence: 99%
“…These programs are now used to perform the structural internal force responses prediction of the Tsing Ma suspension Bridge with a main span of 1377m. The aerodynamic and aeroelastic parameters of bridge deck are taken from the wind tunnel test results (Zhu, 2002) and the reference mean wind speed is taken as 25m/s. The studied cases are listed in table 1.…”
Section: Random Vibration Methodsmentioning
confidence: 99%
“…Equations (5)- (7) is expressed in a frequency manner for complex sinusoidal structural motions [33], but the self-excited forces can be reshaped as aerodynamic stiffness and aerodynamic damping [6,9,34,35]. Hence, the governing equation by Equation (1) can be further expressed as …”
Section: H(t)mentioning
confidence: 99%
“…In this study, this number will be odd considering the distribution in Figure 13a. The relationship between N and subscript n can be expressed as Equation (9). When the other parameters are given, more TMDs will lead to more intensive natural frequencies.…”
Section: Design Parameters Of the Mtmdmentioning
confidence: 99%
“…Therefore, it is necessary to take into account the mechanical nonlinear behaviors when studying aerodynamic or aeroelastic performances of bluff bodies via SSSM tests, because the aerodynamic and aeroelastic parameters used in the research are commonly identified through identification of system parameters and by subtracting the mechanical damping and stiffness obtained in the still air condition from the overall ones identified under the flowing air (i.e. wind) conditions [1,[5][6][7][8]. Therefore, neglecting mechanical nonlinearities will undoubtedly introduce the modeling errors of mechanical damping and stiffness into the identification results of aerodynamic parameters, which is likely one of the main causes of frequent dispersion of identified flutter derivates at high reduced wind speed [2,5], where large initial excitations are needed to get long-duration signals of free decay vibrations.…”
Section: Introductionmentioning
confidence: 99%