A numerical and experimental investigation of delamination behaviour in the DCB specimen
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: Fatigue and fracture mechanics · Mechanical Behavior of Composites · Structural Response to Dynamic Loads
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (26)
Show source-provided references
1. Round robin testing for mode I interlaminar fracture toughness of composite materials10.1520/CTR10379J ↗
2. Hashemi S, Kinloch AJ, Williams JG. Proc R Soc Lond A 1990;427:451–459.10.1098/rspa.1990.0007 ↗
3. A simplified improved beam analysis of the DCB-specimen10.1016/0266-3538(92)90056-9 ↗
4. Improved method for calculating strain energy release rate based on beam theory10.2514/3.11965 ↗
5. Delamination characteristics of double-cantilever beam and end-notched flexure composite specimens10.1016/0266-3538(96)00001-2 ↗
6. Schön J, Andersson B. A theoretical study of the DCB and ENF test specimens. To be submitted to Journal of Applied Mechanics.
7. Effect of finite width on deflection and energy release, rate on an orthotropic double cantilever specimen10.1177/002199838802200704 ↗
8. Effect of stacking sequence on energy release rate distributions in multidirectional DCB and ENF specimens10.1016/S0013-7944(96)00037-9 ↗
9. An analytical investigation of delamination front curvature in double cantilever beam specimens10.1177/002199839002401101 ↗
10. On growth of crack fronts in the DCB-tes10.1016/0961-9526(93)90050-T ↗
11. Microfocus radiography studies during mode I interlaminar fracture tests on composites10.1007/BF00728603 ↗
12. Polaha JJ. Effect of interfacial ply orientation on the fracture toughness of a laminated composite, AIAA-94-1537-CP, pp. 1707–16.
13. Effect of mode ratio, ply orientation and precracking on the delamination toughness of a laminated composite10.1177/073168449601500202 ↗
14. Damage propagation in composite structural elements-coupon experiments and analyses10.1016/S0263-8223(96)00078-5 ↗
15. Reliable stress and fracture mechanics analysis of complex components using a h-p version of FEM10.1002/nme.1620381302 ↗
16. European Structural Integrity Society–Polymer and Composite Task Force. Protocol for interlarninar fracture testing Nos. 1 and 2, March 1992.
17. Standard test method for Mode 1 interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites. American Society For Testing and Materials, D 5528 - 94a.
18. Granstam P. Fractographical examination of DCB tested carbon fibre composite samples. A Saab/BAe collaboration, CSM-T5447, 1996.
19. Wilkins DJ, Eisenman JR, Camin RA, Margolis WS, Benson RA.Characterizing delamination growth in graphite-epoxy. Damage in composite materials, ASTM STP 775. American Society for Testing and Materials, 1982. p. 168–83.10.1520/STP34326S ↗
20. The characterisation of Mode I delamination failure in non-woven, multidirectional laminates10.1016/0010-4361(84)90708-0 ↗
21. Krüger R, König M, Schneider T. Computation of local energy release rates along straight and curved delamination fronts of unidirectionally laminated DCB and ENF-specimens. In: Proceedings of the 34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Material Conference, April 1993, p. 1332–42.10.2514/6.1993-1457 ↗
22. Laméris L. The use of load enhancement factor in the certification of composite aircraft structures. National Aerospace Laboratory the Netherlands, NLR TP 90068U.
23. Prinz R, Gädke M. Characterisation of interlaminar mode I and mode II fracture in CFRP laminates. In: Proc. of Inter. Conf. on Spacecraft Structures and Mechanical Testing. ESA SP-321, 1991. p. 97–102.
24. Effect of matrix resin on delamination fatigue crack growth in CFRP laminates10.1016/0013-7944(94)90109-0 ↗
25. Martin RH, Murri GB. Characterization of mode I and mode II delamination growth and thresholds in AS4/PEEK composites. ASTM STP 1990; 1059: 251–70.10.1520/STP24115S ↗
26. Schön J, Nyman T, Blom A, Ansell, H. A numerical and experimental investgation of a composite ENF-specimen. Submitted to Engineering Fracture Mechanics.