D5.4 - Report and data on the effect of fatigue loading history on damage development

Fracture in laminated composites is typically caused by inter-laminar damage, such as delamination, promoted by or coexisting with intra-laminar damage, like matrix-cracking and fibre failure. During operation of composite structures, these damage mechanisms initiate and propagate under variable amplitude loading conditions that are very different from the constant amplitude loading conditions applied to test specimens in laboratories to characterise fatigue properties of the material. The work in Task 5.4 focuses on the effect of variable amplitude loading on the damage evolution in fiber reinforced polymer laminated composites. An experimental test campaign investigates fatigue-driven delamination under multi-level block loading, and a new crack growth rate model is proposed. The crack growth rate model is included in a finite element formulation as an extension of the inter-laminar fatigue damage method from Task 5.1. The method has been implemented in the Simcenter Samcef software. The simulated results from the Simcenter Samcef solver show a significant improvement in the delamination growth prediction in comparison to the conventional non-interaction crack growth rate model. Another experimental campaign investigates intra-laminar damage under two-level block loading. The experiments subject specimens to flexural fatigue loading using a simplified test configuration that can be readily implemented by most any research group with access to a universal fatigue testing machine. The simplified experimental setup used in this work was suitable to investigate the load history effects on intralaminar damage evolution