2021
DOI: 10.1016/j.engstruct.2021.112416
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Fatigue behaviour of composite girders with concrete-filled tubular flanges and corrugated webs—experimental study

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Cited by 15 publications
(6 citation statements)
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“…The crack tip is represented by a half-length ( a ) under remote tensile stress on the flange σ bf referring to a similar finite width plate model in Ref. [ 34 ]. The equilibrium of tensile stress along the z axis for two crack tips and a seam in between can be written as: where e is the eccentricity between the centre of the crack and the centreline of the flange while it can be deduced as 0.5 b l sin θ c .…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…The crack tip is represented by a half-length ( a ) under remote tensile stress on the flange σ bf referring to a similar finite width plate model in Ref. [ 34 ]. The equilibrium of tensile stress along the z axis for two crack tips and a seam in between can be written as: where e is the eccentricity between the centre of the crack and the centreline of the flange while it can be deduced as 0.5 b l sin θ c .…”
Section: Resultsmentioning
confidence: 99%
“…The crack tip is represented by a half-length (a) under remote tensile stress on the flange σbf referring to a similar finite width plate model in Ref. [34]. The equilibrium of tensile stress along the z axis for two crack tips and a seam in between can be written as: For the sake of interpreting the stress state around the crack front of the cracked joint, suppose the centre of the crack coincided with the centreline of the longitudinal fold of the corrugated web adjoining the flange plate, as shown in Figure 7.…”
Section: Numerical Verificationmentioning
confidence: 99%
“…The shape of the border components has a considerable impact on the structure's quasi-static behaviour [14]. Fatigue crack initiation is correctly accounted for at the top surface of the bottom tubular flange, where longitudinal stress accumulates at the welded toes towards the end of the inclined fold adjoining longitudinal fold of the corrugation [15], [16]. Very stiff springs are used to mimic the geometric limitations of the folded plates, such as the conditions at the ends and intermediate supports [17]- [22].…”
Section: Introductionmentioning
confidence: 99%
“…Accordingly, fatigue cracks usually originate in the joint between the CSWs and the top slab [ 12 , 13 , 14 ]. To predict the potential fatigue failure of composite beams with CSWs, calculation methods for the fatigue life have been investigated by many researchers as well [ 15 , 16 , 17 ].…”
Section: Introductionmentioning
confidence: 99%