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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Zeisberg, Marcel
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document
Investigating the VHCF of composite materials using new testing methods and a new fatigue damage model
Abstract
Composite materials are used in several fatigue-relevant applications nowadays and characteristicfatigue data is needed. However, composites have to be told apart from metals and so have to be the fatiguebehaviors. Unfortunately, the established testing and simulation methods are not suitable for composites.However, two new experimental approaches providing accelerated VHCF testing are presented. A resonantand a non-resonant setup are used. For the first setup the resonant behavior of specimen and test stand areused to load GFRP tubes at roughly 600Hz and a load ratio of R=-1. The second approach utilizes aspecifically designed four-point bending test running at 50-80 Hz. Fatigue data including stiffnessdegradation, evaluation of crack density and delamination are gained up to10 8 cycles. Both methods reachtesting frequencies beyond classic testing methods and thus allow time efficient VHCF testing. First resultsfor fatigue testing with glass-fiber-reinforced plastics are presented.Furthermore, a new layer-based fatigue damage model (FDM) is presented, which is physically motivated byusing an approach that relates energy dissipated under quasi-static and the energy dissipated under cyclicloading. The Puck failure criterion is used and has been extended with degradation factors for analyzingdiscontinuous damage. Load interactions as well as nonlinear damage accumulation are taken into account.Degradation of stiffness and strength can be calculated for every single layer over the simulated lifetime.