Delamination of a composite laminated under monotonic loading

被引：3

作者：

Achache, Habib ^{[1
]}

Benzerdjeb, Abdelouahab ^{[2
]}

Mehidi, Abdelkader ^{[3
]}

Boutabout, Benali ^{[3
]}

Ouinas, Djamel ^{[4
]}

机构：

[1] Univ Dr Yahia Fares Medea, Dept Mat Engn, Urban Pole, Medea 26000, Algeria

[2] Univ Sci & Technol Oran Mohammed Boudiaf USTO, Dept Mech Engn, BP1505 El Menaouar, Oran 31036, Algeria

[3] Univ Djillali Liabes Sidi Bel Abbes, LMPM, BP 89,St Ben MHidi, Sidi Bel Abbes, Algeria

[4] Univ Mostaganem, Lab Numer & Expt Modeling Mech Phenomena, Route Belahcel, Mostaganem 27000, Algeria

来源：

STRUCTURAL ENGINEERING AND MECHANICS | 2017年 / 63卷 / 05期

关键词：

cracks; delamination; stress intensity factor; fibers orientations; finite element method and laminates; MULTIPLE DELAMINATIONS; COMPRESSIVE FAILURE; CRACK-GROWTH; MODE-I; BEHAVIOR; PLATES; BEAMS;

D O I：

10.12989/sem.2017.63.5.597

中图分类号：

TU [建筑科学];

学科分类号：

0813 ;

摘要：

Our work aims to analyze using the finite element method the evolution of the stress intensity factor (SIF) parameter K of three laminated folded plates stacks [+alpha, -alpha], made of the same epoxy matrix and different reinforcement fibers (boron, graphite and glass). Our results show that the angle of orientation of the boron/epoxy composite has no great influence on the variation of the parameter KI. Compared to composite graphite/epoxy and glass/epoxy, the laminated composite boron/epoxy reduces more the SIF KI in the middle of the plate for angles 0 degrees <=alpha <= 30 degrees.

引用

页码：597 / 605

页数：9

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