The tendency for free-edge delamination in laminates and its minimization
Source abstract
Abstract
The laminate free-edge effect may have a detrimental impact on the effective strength of composite laminates. The reason for this is the occurrence of high interlaminar stresses in the immediate vicinity of free edges which are not taken into acccount by the classical theory of thin laminates. The present paper is devoted to a systematic reduction of the free-edge delamination tendency by structural optimization methods where different approaches are used for the assessment of the delamination tendency. In addition to considering the effective delamination moments as a result of the classical laminate theory, the free-edge stresses are calculated by the finite-element method and by a closed-form analytical approach. Furthermore an energy release criterion is used.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Mechanical Behavior of Composites · Composite Structure Analysis and Optimization · Aeroelasticity and Vibration Control
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (11)
Show source-provided references
1. Jones · 1975
2. Interlaminar stresses in composite laminates under uniform axial extension10.1177/002199837000400409 ↗
3. Free edge effects in laminated composites
4. Estimation of transverse/interlaminar stresses in laminated composites—a selective review and survey of current developments10.1016/S0263-8223(99)00126-9 ↗
5. An efficient method for the calculation of interlaminar stresses in composite materials10.1115/1.3171853 ↗
6. Stiftinger MA. Semi-analytical finite element formulations for layered composite shells with consideration of edge effects. Fortschritt-Berichte VDI, Reihe 18, Nr. 203. Düsseldorf: VDI-Verlag, 1996.
7. Interlaminar stresses at the free corners of a laminate10.1016/S0263-8223(99)00019-7 ↗
8. Fracture mechanics using a 3D composite element10.1016/S0263-8223(99)00011-2 ↗
9. A finite element calculation of stress intensity factors by a modified crack closure integral10.1016/0013-7944(77)90013-3 ↗
10. Jacob · 1982
11. Vanderplaats · 1984