journal article·2000-03

Initiation and bifurcation mechanisms of cracks in multi-directional laminates

A. Laksimi, A. Ahmed Benyahia, M.L. Benzeggagh, X.L. Gong

Composites Science and Technology· Volume 60· Issue 4
Publisher page

Abstract

Abstract This work studies the behaviour of multidirectional composite laminate under opening (mode I) loading. The material used is a glass/epoxy composite. The stacking sequence ± θ was selected to minimise coupling effects. The experimental results showed that several fracture modes depend on the angle of the ply orientation and on the applied stress type. For small angles ( θ ⩽30°), the fracture type is delamination on the mid plane. For large angles ( θ >67°), the fracture takes place by flexure at the head of the precrack. For the intermediate angles, the bifurcation phenomenon leads to a delamination in staircase.
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Research context

OpenAlex topics: Mechanical Behavior of Composites · Structural Analysis of Composite Materials · Composite Structure Analysis and Optimization

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (17)

Show source-provided references
1. Russell AJ, Street KN. Factors affecting the interlaminar fracture energy of graphite/epoxy laminates. In: Hayashi J, Kawata K, Umekawa S, editors. Progress in science and engineering of composites. ICCM IV, Tokyo, 1982. p. 279–300.
2. Effects of lay-up temperature and loading rate in DCB test of interlaminar crack growth10.1520/CTR10810J ↗
3. Ramkunar RL, Whitcomb JD. Characterization of mode I and mixed mode delamination growth in T300/5208 graphite/epoxy. In: Johnson WS, editor. ASTM STP 775, 1985. p. 315–35.10.1520/STP36312S ↗
4. Wilkins DJ, Eisenmann JR, Camin RA, Margolis WS, Benson RA. Characterizating delamination growth in graphite/epoxy. In: Damage in composite materials, ASTM STP 775. Phildelphia: ASTM, 1982. p. 168–83.
5. delamination failure in non-wowen, multidirectional laminates10.1016/0010-4361(84)90708-0 ↗
6. Mode I interlaminar fracture of symmetrical cross-ply composites10.1016/0266-3538(91)90025-K ↗
7. Effect of finite width on deflection and energy release rate of an orthotropic double cantiliver specimen10.1177/002199838802200704 ↗
8. Technique for predicting mode I energy release rates using a first-order shear deformable plate theory10.1016/0013-7944(90)90105-P ↗
9. An analytical investigation of delamination front curvature in double cantiliver beam specimens10.1177/002199839002401101 ↗
10. Delamination characteristics of double cantiliver beam and end-notched flexure composite specimens10.1016/0266-3538(96)00001-2 ↗
11. Microfocus radiography studies during mode I interlaminar fracture test on composites10.1007/BF00728603 ↗
12. End corrections for orthotropic D.C.B specimens10.1016/0266-3538(89)90058-4 ↗
13. Associated path independent J integrals for separating mixed modes10.1016/0022-5096(83)90010-8 ↗
14. Rybicki EF, Kanninen MF. A finite element in linear fracture mechanics. Int. J Numer Meth Eng 10:25–35.10.1002/nme.1620100103 ↗
15. Determination of GIC in angle ply composites using a cantiliver beam test method10.1177/073168448300200101 ↗
16. Local delamination in laminates with angle ply matrix cracks, part I
17. Tsai SW. Theory of composites design. Think Composites, 1992 (Section 8).