A double-plate finite-element model for the impact-induced delamination problem
Bibliographic record
Abstract
No abstract is available for this record. The assistant can identify its topic from the title, but cannot infer the study’s results.
Source: Not provided · Quality: missing
Research context
OpenAlex topics: Mechanical Behavior of Composites · Structural Response to Dynamic Loads · Composite Structure Analysis and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (20)
Show source-provided references
1. A quasi-static treatment of delamination crack propagation in laminates subjected to low velocity impact
2. Limits of quasi-static solutions in impact of composite structures10.1016/0961-9526(92)90009-U ↗
3. A model for predicting damage in graphite/epoxy laminate composites resulting from low velocity impact10.1177/002199839202601408 ↗
4. Strain energy release rate distribution for double cantilever beam specimen10.2514/3.10791 ↗
5. Delaminations in composite plates under transverse static or impact loads—a model10.1016/0263-8223(93)90221-B ↗
6. FEM study on the interface crack in layered composite materials
7. Delamination and matrix cracking of cross-ply laminates due to a spherical indenter10.1016/0263-8223(93)90172-M ↗
8. Computation of strain energy release rate for skin-stiffener debonds modeled with plate elements
9. Computational method for using plate elements in skin-stiffener debonding analysis
10. Fracture mechanics analysis of composite skin-stiffener debond configurations with shell elements
11. A plate finite element for modelling delamination10.1177/073168449301200208 ↗
12. Strain energy release rate distribution along a delamination front using plate theory
13. On interface crack growth in composite plates10.1115/1.2893756 ↗
14. A finite element calculation of stress intensity factors by a modified crack closure integral10.1016/0013-7944(77)90013-3 ↗
15. IMSL Math/Library · Version 1.0. MALB-USMPERFCT-1.0 · 1987
16. Improved method for calculating strain energy release rate based on beam theory10.2514/3.11965 ↗
17. On strain energy release rates for interfacial cracks in bi-material media10.1016/0013-7944(87)90115-9 ↗
18. Effect of adhesive layers on impact damage in composite laminates
19. Finn · 1991
20. On large deflection effects in unsymmetric cross-ply composite laminates10.1177/002199838802201103 ↗