| Revista: | Materials research |
| Base de datos: | PERIÓDICA |
| Número de sistema: | 000312888 |
| ISSN: | 1516-1439 |
| Autores: | Tarpani, Jose Ricardo1 Milan, Marcelo Tadeu Spinelli, Dirceu Bose, Waldek Wladimir |
| Instituciones: | 1Universidade de Sao Paulo, Escola de Engenharia, Sao Carlos, Sao Paulo. Brasil |
| Año: | 2006 |
| Periodo: | Abr-Jun |
| Volumen: | 9 |
| Número: | 2 |
| Paginación: | 121-130 |
| País: | Brasil |
| Idioma: | Inglés |
| Tipo de documento: | Nota breve o noticia |
| Enfoque: | Experimental |
| Resumen en inglés | In Part II of this work, quasi-static tensile properties of four aeronautical grade carbon-epoxy composite laminates, in both the as-received and pre-fatigued states, have been determined and compared. Quasi-static mechanical properties assessed were tensile strength and stiffness, tenacity (toughness) at the maximum load and for a 50% load drop-off. In general, as-molded unidirectional cross-ply carbon fiber (tape) reinforcements impregnated with either standard or rubber-toughened epoxy resin exhibited the maximum performance. The materials also displayed a significant tenacification (toughening) after exposed to cyclic loading, resulting from the increased stress (the so-called wear-in phenomenon) and/or strain at the maximum load capacity of the specimens. With no exceptions, two-dimensional woven textile (fabric) pre-forms fractured catastrophically under identical cyclic loading conditions imposed to the fiber tape architecture, thus preventing their residual properties from being determined |
| Disciplinas: | Ingeniería |
| Palabras clave: | Ingeniería de materiales, Ingeniería mecánica, Carbono/epoxi, Láminas, Aeronáutica, Propiedades mecánicas, Fatiga de materiales, Resistencia |
| Keyword: | Engineering, Materials engineering, Mechanical engineering, Carbon/epoxy, Laminates, Aeronautics, Mechanical properties, Materials fatigue, Resistance |
| Texto completo: | Texto completo (Ver HTML) |
