Tapered laminates under static and fatigue tension loading

Composites Science and Technology

Volumn 62, Issue 4, 2002, Pages 597-603

  Meirinhos, G ^a   Rocker, J ^b   Cabanac, J P ^b   Barrau, J J ^a  

^a UNIVERSITÉ DE TOULOUSE   (France)

^b AIRBUS   (France)

Author keywords

A. Carbon fibers; B. Fatigue; C. Delamination; C. Statistics; Ply drop off

Indexed keywords

CARBON FIBERS; DELAMINATION; FATIGUE OF MATERIALS; FATIGUE TESTING; LAMINATED COMPOSITES; STATISTICAL METHODS; STRENGTH OF MATERIALS; TENSILE TESTING;

TAPERED LAMINATES;

CARBON CARBON COMPOSITES;

CARBON FIBER; DELAMINATION; FATIGUE; FIBER REINFORCED COMPOSITE; LOADING; TENSION;

EID: 0036500231     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0266-3538(01)00156-7     Document Type: Article

References (3)

1. Fatigue and damage tolerance for the certification of composite structures of civil aircraft