Fractography analysis and fatigue strength of carbon fiber/RTM6 laminates

Materials Science and Engineering: A

Volumn 527, Issue 15, 2010, Pages 3609-3614

  Cioffi, Maria Odila Hilário ^a   Voorwald, Herman Jacobus Cornelis ^a   Camargo, José André Marin ^a   Rezende, Mirabel Cerqueira ^b   Ortiz, Edmundo C ^c   Ambrosio, Luigi ^d  

^a SÃO PAULO STATE UNIVERSITY UNESP   (Brazil)

^b INSTITUTO DE AERONÁUTICA E ESPAÇO   (Brazil)

^c INSTITUTO TECNOLÓGICO DE AERONÁUTICA   (Brazil)

^d CNR   (Italy)

Author keywords

Aluminum alloys; Composites; Electron microscopy; Fatigue

Indexed keywords

AIRFRAMES; ALUMINUM ALLOYS; CARBON FIBERS; FRACTURE MECHANICS; LANDING GEAR (AIRCRAFT); RESIN TRANSFER MOLDING;

COMPOSITE AIRFRAME; EXPERIMENTAL METHODOLOGY; FATIGUE STRENGTH; HIGH QUALITY; LOW-COSTS; MANUFACTURING PROCESS; MOLDING PROCESS; POLYMER COMPOSITE; RESIN-TRANSFER MOLDING; SIMPLE GEOMETRIES;

FATIGUE TESTING;

EID: 77950865356     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.msea.2010.02.054     Document Type: Article

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