journal article·2010-08Open access

Tensile strength of UD-composite laminates with multiple holes

S. Kazemahvazi, J. Kiele, D. Zenkert

Composites Science and Technology· Volume 70· Issue 8

Abstract

The residual strength of glass fibre reinforced vinyl-ester laminates with multiple holes was investigated through an experimental programme. Different types of structured hole patterns and hole densities were investigated and analysed using digital image correlation strain measuring technique. Three different failure modes could be observed when the hole patterns and the hole densities were a altered. These three failure modes were used as the foundation for a simple yet effective analytical model in order to predict the residual strength of damaged composite specimens. Finally, a number of laminates with randomly distributed holes were tested experimentally. The analytical model can predict the failure mode and failure strength of the experiments with sufficiently good fidelity.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Fatigue and fracture mechanics · Optical measurement and interference techniques

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

References (14)

Show source-provided references
1. A constitutive model for anisotropic damage in fiber-composites10.1016/0167-6636(94)00053-0 ↗
2. Failure criteria for unidirectional fiber composites10.1115/1.3153664 ↗
3. Maimi P, Camanho PP, Mayugo J, Davila CG. A thermodynamically consistent damage model for advanced composites. Technical report NASA/TM-2006-214282; 2006.
4. Progressive damage modelling in fiber-reinforced materials10.1016/j.compositesa.2007.01.017 ↗
5. Numerical and experimental analysis of the interaction between two notches in carbon fibre laminates10.1016/j.compscitech.2007.07.023 ↗
6. Notch and strain rate sensitivity of non-crimp fabric composites10.1016/j.compscitech.2008.06.002 ↗
7. Fracture strength in randomly perforated plates10.1063/1.2733623 ↗
8. Tensile strength of randomly perforated aluminium plates: Weibull distribution parameters10.1063/1.2948942 ↗
9. Stresses concentration of finite composite laminates weakened by multiple elliptical holes10.1016/0020-7683(94)00301-C ↗
10. Stress analysis of finite composite laminate with multiple loaded holes10.1016/S0020-7683(97)00343-0 ↗
11. Strength prediction of composite laminates with multiple elliptical holes10.1016/S0020-7683(99)00033-5 ↗
12. Reichold AS, Preliminary data sheet, NORPOL Dion 9500; 02.2000.
13. Devold AMT AS, Product information, N-6030 Langevåg, Norway; 04.2000. .
14. GOM Aramis, theory and user manual; 2006. .