journal article·2004-08

A step-size independent method for finite element modeling of damage in composites

J.C. Zarco-González, N.A. Fellows, J.F. Durodola

Composites Science and Technology· Volume 64· Issue 10-11
Publisher page

Abstract

The solutions of damage progression models are known to be highly step-size dependent. This paper develops a new algorithm to predict damage, within a problem at a given load, which is not step size dependant. Two different cases have been studied using the current load incremented solution methods and the new algorithm. The algorithm is shown to produce similar results when compared to the load incremented solution methods, when they utilise a small enough step size to ensure a converged solution. It is therefore concluded that the new failure algorithm can save time by providing confidence that a correctly converged solution has been found without the need to carry out an iterative check on the effect of step size.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Probabilistic and Robust Engineering Design · Fatigue and fracture mechanics

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

References (11)

Show source-provided references
1. Failure strength of nonlinearly elastic composite laminates a pin loaded hole10.1177/002199838401800506 ↗
2. A progressive damage model for laminated composites containing stress concentration10.1177/002199838702100904 ↗
3. Post-failure analysis of bolted composite joints in tension or shear-out mode failure10.1177/002199838702100903 ↗
4. Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings part I – analysis10.1177/002199839102500101 ↗
5. Strength envelope of bolted composite joints under by-pass loads10.1177/002199839603001301 ↗
6. Numerical and experimental failure analysis of composite laminates with bolted joints under bending loads10.1177/002199839502900102 ↗
7. Bearing failure of bolted composite joints, part II: model and verification10.1177/002199839603001204 ↗
8. Three-dimensional stress analysis of bolted single-lap composite joints10.1016/S0263-8223(98)00103-2 ↗
9. ABAQUS/Standard Example Problems Manual, Vol. 1, Version 6.2 S
10. Feih S, Shercliff HR, McGrath G. 3-d Progressive damage modelling for adhesively bonded composite peel joints: implementation in a UMAT and related computational issues. In: Conference Proceedings ABAQUS UK User Conference, 2000
11. A progressive failure model for composite laminates containing opening10.1177/002199839102500505 ↗