2019
DOI: 10.1061/(asce)cc.1943-5614.0000959
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In-Plane Shear Characterization of Composite GFRP-Foam Sandwich Panels

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Cited by 6 publications
(4 citation statements)
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“…Since the loading conditions were the same, the failure mode of the honeycomb sandwich panel was identical to that of the foam sandwich panels. 29 Due to the larger bonding area between the foam core and the skins, the extent of delamination was smaller than that in honeycomb sandwich panels.…”
Section: Unrepaired Specimenmentioning
confidence: 99%
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“…Since the loading conditions were the same, the failure mode of the honeycomb sandwich panel was identical to that of the foam sandwich panels. 29 Due to the larger bonding area between the foam core and the skins, the extent of delamination was smaller than that in honeycomb sandwich panels.…”
Section: Unrepaired Specimenmentioning
confidence: 99%
“…Picture frame test is a kind of experimental tests for characterizing the material behavior of textile composites. In recent years, the frame test has been widely used to measure the shear properties of carbon/glass fiber composite laminates and plain weave fabrics 27–32 . DIC system is a good choice for measuring the strain of sandwich panels.…”
Section: Introductionmentioning
confidence: 99%
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“…In the case of shear, the deformable square bench applied to sandwich panel is proposed by ASTM standard D8067. The method is used in [21] to assess the core inplane shear load contribution to failure modes and especially global buckling. The standard is reliable to obtain the in-plane shear properties of sandwich structures with a special focus on proper hinge mechanisms around the four corners.…”
Section: Introductionmentioning
confidence: 99%