COCOMAT - Improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapse

Composite Structures

Volumn 73, Issue 2, 2006, Pages 175-178

  Degenhardt, Richard ^a   Rolfes, Raimund ^b   Zimmermann, Rolf ^a   Rohwer, Klaus ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b LEIBNIZ UNIVERSITY HANNOVER   (Germany)

Author keywords

Buckling; Collapse; Composites; Degradation; Experiments; Postbuckling; Simulation tools; Skin stringer separation

Indexed keywords

AIRFRAMES; BUCKLING; COMPOSITE STRUCTURES; SIMULATION; STRUCTURAL DESIGN; STRUCTURAL LOADS;

COLLAPSE; FIBRE COMPOSITE FUSELAGE STRUCTURES; LOAD-DISPLACEMENT-CURVE; POSTBUCKLING; SIMULATION TOOLS; SKIN-STRINGER SEPARATION;

FUSELAGES;

AIRCRAFT;

EID: 32044471533     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2005.11.042     Document Type: Article

References (2)

1. Zimmermann R, Rolfes R. POSICOSS - Improved postbuckling simulation for design of fibre composite stiffened fuselage structures. Composite Structures.
2. www.posicoss.de.