An empirical modified fatigue damage model for impacted GFRP laminates

作者：Naderi S; Hassan M A^*; Bushroa A R

来源：Acta Astronautica, 2014, 103: 119-128.

DOI：10.1016/j.actaastro.2014.06.028

• Fatigue
• Failure-model
• Low-velocity-impact
• Residual-strength
• GFRP

The aim of the present paper is to evaluate the residual strength of GFRP laminates following a low-velocity impact event under cyclic loading. The residual strength is calculated using a linear fatigue damage model. According to an investigation into the effect of low-velocity impact on the fatigue behavior of laminates, it seems laminate fatigue life decreases after impact. By normalizing the fatigue stress against undamaged static strength, the Fatigue Damage parameter "FD" is presented with a linear relationship as its slope which is a linear function of the initial impact energy; meanwhile, the constants were attained from experimental data. FD is implemented into a plane-stress continuum damage mechanics based model for GFRP composite laminates, in order to predict damage threshold in composite structures. An S-N curve is implemented to indicate the fatigue behavior for 2 mm thickness encompassing both undamaged and impacted samples. A decline in lifespan is evident when the impact energy level increases. Finally, the FD is intended to capture the unique GFRP composite characteristics.

• 出版日期2014-11