journal article·1994-01

Synergism between layer cracking and delaminations in multidirectional laminates of carbon-fibre-reinforced epoxy

H. Eggers, H.C. Goetting, H. Bäuml

Composites Science and Technology· Volume 50· Issue 3
Publisher page

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: Smart Materials for Construction · Mechanical Behavior of Composites · Structural Behavior of Reinforced Concrete

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (20)

Show source-provided references
1. Mechanical properties and damage mechanismsof carbonfibre-reinforced composites, Tension loading
2. Initiation and propagation of cracks in notched UD-laminates of carbonfibre-reinforced epoxy under static testile load
3. Querriβbildung in 0/90/0 CFK-Laminaten10.1002/mawe.19870180909 ↗
4. Application of Paris equation to the fatigue growth of transverse ply cracks10.1177/002199838902300706 ↗
5. Difference in the failure process of CFRP and GFRP-cross-ply laminates
6. The strain energy release rate of composite microcracking: A variational approach10.1177/002199838902301102 ↗
7. A simplified analysis of transverse ply cracking in cross-ply laminates10.1016/0266-3538(88)90008-5 ↗
8. Transverse cracking and stiffness reduction in composite laminates10.1177/002199838501900404 ↗
9. Progressive transverse cracking in composite laminates10.1177/002199838802201001 ↗
10. Constitutive relations of a cracked composite lamina10.1177/002199838802200401 ↗
11. Damage mechanisms and constitutive relations for cracked UD-layers in cross-ply laminates
12. Mechanical properties and damage mechanics of carbonfibre-reinforced composites, Compression loading
13. Einflusb der Randdelaminationsbehinderung in multidirektionalen CFK-Laminaten unter Zugschwellbelastung
14. Analysis of fatigue damage in composite laminates10.1016/0142-1123(80)90022-5 ↗
15. Crack development in graphite-epoxy cross-ply laminates under uniaxial tension10.1016/0266-3538(85)90058-2 ↗
16. Delamination crack originated from transverse cracking in cross-ply composite laminates under extension10.1016/0020-7683(91)90186-J ↗
17. Fracture/damage mechanics of composites, Static and fatigue properties
18. Load and failure analyses of CFRP-laminates by means of electrical resistivity measurements10.1016/0266-3538(89)90016-X ↗
19. Standardisierter Einzelflugbelastungsablauf für Schwingfestigkeitsversuche an Tragflächenbauteilen von Transportflugzeugen
20. Mixed mode strain energy release rate effects on edge delaminations of composites