A Micromechanics-Based Damage Model for [± θ / 90n ]s Composite Laminates
| Resumo |
A new damage model based on a micromechanical analysis of cracked [± θ / 90n ]s laminates subjected to multiaxial loads is proposed. The model predicts the onset and accumulation of transverse matrix cracks in uniformly stressed laminates, the effect of matrix cracks on the stiffness of the laminate, as well as the ultimate failure of the laminate. The model also accounts for the effect of the ply thickness on the ply strength. Predictions relating the elastic properties of several laminates and multiaxial loads are presented NASA/TM-2006-214285 |
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| Identificador | |
| Idioma(s) |
eng |
| Publicador |
National Aeronautics and Space Administration |
| Direitos |
Tots els drets reservats |
| Palavras-Chave | #Micromecànica #Micromechanics #Materials compostos -- Fatiga #Composite materials -- Fatigue #Resistència de materials #Strength of materials |
| Tipo |
info:eu-repo/semantics/article info:eu-repo/semantics/publishedVersion |
