2009
DOI: 10.4236/eng.2009.13019
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Effect of Low Velocity Impact Damage on Buckling Properties

Abstract: The work described herein consists of experimental measurement of the post-impact buckling loads of Eglass/epoxy laminates. Composite samples with stacking sequence of [+45/45/90/0] 2s were subjected to low-velocity impact loading at energy levels of 36, 56.13, 79.95, 110.31 and 144 J. The impact tests were conducted with a specially developed vertical drop weight testing machine. Impact parameters like peak load, absorbed energy, deflection at peak load and damage area were evaluated and compared. Damaged sp… Show more

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Cited by 7 publications
(7 citation statements)
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“…These kinds of impact loads can be modeled with various dynamic tests, of which the falling weight impact test is the most commonly used. Figure 9 shows the general layout of such a measuring device 8,94,105 …”
Section: Investigating Methods Of Polymer Foamsmentioning
confidence: 99%
See 2 more Smart Citations
“…These kinds of impact loads can be modeled with various dynamic tests, of which the falling weight impact test is the most commonly used. Figure 9 shows the general layout of such a measuring device 8,94,105 …”
Section: Investigating Methods Of Polymer Foamsmentioning
confidence: 99%
“…General layout of a falling weight impact tester. Reproduced under terms of the CC‐BY license 105 . Copyright 2021, Scientific Research Publishing …”
Section: Investigating Methods Of Polymer Foamsmentioning
confidence: 99%
See 1 more Smart Citation
“…The integral area under the load-displacement curve can be considered as the work the composite laminates applied onto the impactor. In general, the energy absorbed by the samples is designated as the difference between the energy at the end of the impact process and the energy at the maximum load point [34]. Because the CFRP composites are rigid, the energy before reaching the maximum load is considered to be absorbed by the elastic deformation, only the energy after the maximum load is devoted to producing damage.…”
Section: Characterization Of Impact Loads and Energiesmentioning
confidence: 99%
“…These impact loads are considered extremely dangerous and cause invisible damage to the back face or within the laminate which consequently reduce the strength of the composite material, even when the impact produces low energy. It has been proven that if a composite plate is subjected to a low velocity impact, the damaged area will increase with the increase of the impact velocity [ 1 ]. Caprino et al [ 2 ] concluded that the first failure point in a laminated composite plate is influenced more by the impact speed rather than the impacting energy.…”
Section: Introductionmentioning
confidence: 99%