Ítem
|
Turon Travesa, Albert
Costa i Balanzat, Josep Camanho, Pedro Manuel Ponces Rodrigues de Castro Dávila, Carlos G. |
|
| 5 juny 2018 | |
| A damage model for the simulation of delamination propagation under high-cycle fatigue loading is proposed. The basis for the formulation is a cohesive law that links fracture and damage mechanics to establish the evolution of the damage variable in terms of the crack growth rate dA/dN. The damage state is obtained as a function of the loading conditions as well as the experimentally-determined coefficients of the Paris Law crack propagation rates for the material. It is shown that by using the constitutive fatigue damage model in a structural analysis, experimental results can be reproduced without the need of additional model-specific curve-fitting parameters | |
| http://hdl.handle.net/2072/320356 | |
| eng | |
| National Aeronautics and Space Administration | |
| Tots els drets reservats | |
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Materials laminats
Laminated materials Materials compostos Composite materials Materials compostos -- Mètodes de simulació Composite materials -- Simulation methods Materials compostos -- Deslaminatge Composite materials -- Delamination |
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| Simulation of Delamination Propagation in Composites Under High-Cycle Fatigue by Means of Cohesive-Zone Models | |
| info:eu-repo/semantics/article | |
| Recercat |
