Degradation investigation in a postbuckling composite stiffened fuselage panel
- 13 January 2007
- journal article
- Published by Elsevier BV in Composite Structures
- Vol. 82 (2), 217-224
- https://doi.org/10.1016/j.compstruct.2007.01.012
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- COCOMAT—improved material exploitation of composite airframe structures by accurate simulation of postbuckling and collapseComposite Structures, 2006
- Buckling and postbuckling of stringer stiffened fibre composite curved panels – Tests and computationsComposite Structures, 2006
- Experiments on Axial Compression Postbuckling Behavior of Stiffened Cylindrical Composite PanelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2003
- The analysis of skin-to-stiffener debonding in composite aerospace structuresComposite Structures, 2002
- Numerical and experimental investigation of a composite ENF-specimenEngineering Fracture Mechanics, 2000
- A numerical and experimental investigation of delamination behaviour in the DCB specimenComposites Science and Technology, 2000
- Postbuckling behavior of selected curved stiffened graphite-epoxy panels loaded in axial compressionAIAA Journal, 1988
- Postbuckling Behavior of Composite Shear WebsAIAA Journal, 1981