2019
DOI: 10.3390/ma12071127
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Experimental Investigations of Impact Damage Influence on Behavior of Thin-Walled Composite Beam Subjected to Pure Bending

Abstract: The paper deals with buckling, postbuckling, and failure of pre-damaged channel section beam subjected to pure bending. The channel section beams made of eight-layered GFRP laminate with different symmetrical layups have been considered. The specimens with initially pre-damaged web or flange were investigated to access the influence of impact damage on work of thin-walled structure in the full range of load till failure. The bending tests of initially pre-damage beams have been performed on a universal tensile… Show more

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Cited by 11 publications
(11 citation statements)
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“…Among the others, few include publications on research and numerical analyses of even unreinforced beams made of cold-formed Z [ 11 , 12 , 13 ], channel [ 14 ], or sigma [ 15 ] cross-sections. Recently, there have also been some works demonstrating bending in the case of composite beams [ 16 ].…”
Section: Introductionmentioning
confidence: 99%
“…Among the others, few include publications on research and numerical analyses of even unreinforced beams made of cold-formed Z [ 11 , 12 , 13 ], channel [ 14 ], or sigma [ 15 ] cross-sections. Recently, there have also been some works demonstrating bending in the case of composite beams [ 16 ].…”
Section: Introductionmentioning
confidence: 99%
“…The model, i.e., geometry, boundary conditions and the way of load appliance has been assumed as close as possible to those in the experimental test stand ( Figure 2). The geometry of the proposed numerical model is very close to those presented in [35].…”
Section: Numerical Modelmentioning
confidence: 61%
“…The material properties of each ply of GFRP laminate are assumed as same as they were determined in experimental tests and presented in Table 1. It should be added that in case when all layers have the fiber direction inclined to the beam's wall edges ± 45 • the nonlinear even plastic behavior [35] appear in far post-buckling range-does not have any influence on buckling load and post-buckling behavior with small deflection. Considering the above, it was decided to not to take it into the numerical model because it may disturb the analysis of influence of the layer arrangements with elements of ABD laminate stiffness matrix on buckling load, as well as post-buckling behavior and post-buckling stiffness.…”
Section: Numerical Modelmentioning
confidence: 99%
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“…There are many papers based on theoretical approach of thermal analysis on structures whose accomplishments are included in [ 23 , 24 , 25 , 26 , 27 , 28 , 29 ]. Theoretical or/and experimental studies involving the pre- and post-buckling state of thin-walled structures were widely discussed in [ 30 , 31 , 32 , 33 , 34 , 35 , 36 , 37 , 38 , 39 ]. These works concern mainly the structures built of plane plates where the phenomenon of stability was under investigation.…”
Section: Introductionmentioning
confidence: 99%