Fracture of Laminated Rectangular Bar After Buckling

Žiliukas, A.; Malatokienė, Aušra

doi:10.5755/j01.mech.17.4.560

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Cited by 3 publications

(2 citation statements)

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“…Delamination is one of the predominant forms of damage in laminated composite due to the lack of reinforcement through the thickness. The mechanisms of delamination and the evaluation of strength criteria are complex [1]. It is widely recognised that the major contribution to delamination fracture resistance is given by the damage developing in matrix-rich interlaminar layer.…”

Section: Introductionmentioning

confidence: 99%

Effect of Natural Load on Delamination Behaviour of a New Hybrid Woven Composite

Benzerga¹,

Haddi

Lavie

2012

mech

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Section: Introductionmentioning

confidence: 99%

Effect of Natural Load on Delamination Behaviour of a New Hybrid Woven Composite

Benzerga¹,

Haddi

Lavie

2012

mech

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“…They are based on different principles and differ by sophistication level of the hardware and software applied [4][5][6]. As the methods applied, the methods of visual inspection, laser, ultrasonic, acoustic emission, vibration methods, mechanical loading, thermo graphic, thermal emission and other methods can be applied [7,8].…”

Section: Introductionmentioning

confidence: 99%

Structural Integrity Verification of Polycarbonate Type Personal Identity Do-Cuments

Greičius

Daniulaitis

Vasiliauskas

et al. 2012

mech

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Mode III Stress Intensity Factors of Surface Crack in Round Bars

Ismail

Ariffin

Abdullah

et al. 2011

AMR

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This study presents a numerical investigation on the stress intensity factors (SIF), K of surface cracks in round bars that were obtained under pure torsion loadings or mode III. ANSYS finite element analysis (FEA) was used to determine the SIFs along the crack front of surface cracks embedded in the solid circular bars. 20-node isoparametric singular elements were used around the crack tip by shifting the mid-side node ¼-position close to a crack tip. Different crack aspect ratio, a/b were used ranging between 0.0 to 1.2 and relative crack depth, a/D were ranged between 0.1 to 0.6. Mode I SIF, KI obtained under bending moment was used to validate the proposed model and it was assumed this proposed model validated for analyzing mode III problems. It was found that, the mode II SIF, FII and mode III SIF, FIII were dependent on the crack geometries and the sites of crack growth were also dependent on a/b and a/D.

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Fracture of Laminated Rectangular Bar After Buckling

Cited by 3 publications

References 10 publications

Effect of Natural Load on Delamination Behaviour of a New Hybrid Woven Composite

Effect of Natural Load on Delamination Behaviour of a New Hybrid Woven Composite

Structural Integrity Verification of Polycarbonate Type Personal Identity Do-Cuments

Mode III Stress Intensity Factors of Surface Crack in Round Bars

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