journal article·2009-09

Delamination growth mechanisms in woven glass fiber reinforced polymer composites under Mode II fatigue loading at cryogenic temperatures

Yasuhide Shindo, Tomo Takeda, Fumio Narita, Nozomi Saito, Shinya Watanabe, Kazuaki Sanada

Composites Science and Technology· Volume 69· Issue 11-12
Publisher page

Abstract

The purpose of this research is to characterize the cryogenic delamination growth behavior in woven glass fiber reinforced polymer (GFRP) composite laminates subjected to Mode II fatigue loading. Mode II fatigue delamination tests were performed at room temperature, liquid nitrogen temperature (77 K) and liquid helium temperature (4 K) using the four-point bend end-notched flexure (4ENF) test method, and the delamination growth rate data for the woven GFRP laminates were obtained. The energy release rate range was determined by the finite element method. Microscopic examinations of the specimen sections and fracture surfaces were also carried out. The present results are discussed to obtain an understanding of the fatigue delamination growth mechanisms in the woven GFRP laminates under Mode II loading at cryogenic temperatures.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Fatigue and fracture mechanics · Textile materials and evaluations

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

References (36)

Show source-provided references
1. ITER R&D: magnets: central solenoid model coil10.1016/S0920-3796(01)00204-6 ↗
2. Irreversible constitutive law for modeling the delamination process using interfacial surface discontinuities10.1016/j.compstruct.2003.11.005 ↗
3. Delamination growth in composites under cyclic loads10.1177/002199839402800803 ↗
4. The characterization of mode I delamination failure in non-woven, multidirectional laminates10.1016/0010-4361(84)90708-0 ↗
5. Interlaminar fracture toughness and toughening of laminated composite materials: a review10.1016/0010-4361(89)90211-5 ↗
6. Cryogenic mechanical properties of CF/polymer composites for tanks of reusable rockets10.1163/156855101753415373 ↗
7. Double cantilever beam measurement and finite element analysis of cryogenic mode I interlaminar fracture toughness of glass-cloth/epoxy laminates10.1115/1.1345527 ↗
8. Analysis of mode I interlaminar fracture and damage behavior of GFRP woven laminates at cryogenic temperatures10.1177/0021998305052029 ↗
9. End-notched flexure testing and analysis of mode II interlaminar fracture behavior of glass-cloth/epoxy laminates at cryogenic temperatures10.1520/CTR10930J ↗
10. Analysis of mode II interlaminar fracture and damage behavior in end notched flexure testing of GFRP woven laminates at cryogenic temperatures10.1007/s00707-006-0357-0 ↗
11. Mode II interlaminar fracture and damage evaluation of GFRP woven laminates at cryogenic temperatures using the 4ENF specimen10.1177/0021998308090451 ↗
12. Mode III interlaminar fracture behavior of glass fiber reinforced polymer woven laminates at 293 to 4K10.1007/s10443-006-9008-9 ↗
13. Analysis and testing of mixed-mode interlaminar fracture behavior of glass-cloth/epoxy laminates at cryogenic temperatures10.1115/1.2019944 ↗
14. Mixed-mode interlaminar fracture and damage characterization in woven fabric-reinforced glass/epoxy composite laminates at cryogenic temperatures using the finite element and improved test methods10.1016/j.engfracmech.2008.07.009 ↗
15. Effect of cryogenic temperature on the fracture toughness of graphite/epoxy composites10.1115/1.2172274 ↗
16. Mode I and II delamination fatigue crack growth behavior of alumina fiber/epoxy laminates in liquid nitrogen10.1016/S0142-1123(01)00065-2 ↗
17. Mode I fatigue delamination growth in GFRP woven laminates at low temperatures10.1016/j.engfracmech.2006.03.015 ↗
18. On the analysis and design of the end notched flexure (ENF) specimen for mode II testing10.1177/002199838602000606 ↗
19. Delamination growth and thresholds in a carbon/epoxy composite under fatigue loading10.1520/CTR10914J ↗
20. Experimental investigation on the influence of crack front to fiber orientation on fatigue delamination growth rate under mode II10.1016/j.compscitech.2005.04.033 ↗
21. JIS K 7086-1993. Testing methods for interlaminar fracture toughness of carbon fibre reinforced plastics; 1993.
22. Mode II fracture toughness evaluation using four point bend, end notched flexure test10.1179/146580199101540565 ↗
23. Numerical evaluation of the effects of friction and geometric nonlinearities on the energy release rate in three- and four-point bend end-notched flexure tests10.1016/j.engfracmech.2005.11.007 ↗
24. A status report on delamination resistance testing of polymer-matrix composites10.1016/j.engfracmech.2007.03.012 ↗
25. Micromechanical analysis of composite laminates at cryogenic temperatures10.1177/0021998305057365 ↗
26. Fracture toughness of transverse cracks in graphite/epoxy laminates at cryogenic conditions10.1016/j.compositesb.2006.06.005 ↗
27. Three-dimensional thermoelastic analysis of cracked plain weave glass/epoxy composites at cryogenic temperatures10.1016/j.compscitech.2004.04.003 ↗
28. A direct energy balance approach for determining energy release rates in three and four point bend end notched flexure tests10.1007/s10704-005-3746-9 ↗
29. A micromechanics model for thermoelastic properties of plain weave fabric composites10.1115/1.2904322 ↗
30. Dahlerup-Petersen K, Perrot A. Properties of organic composite materials at cryogenic temperatures. CERN ISR-BOM/79-39, Geneva, Switzerland; 1979.
31. Cryogenic damage and fracture behaviors of G-11 woven glass-epoxy laminates10.1299/jsmea.48.91 ↗
32. A finite element calculation of stress intensity factors by a modified crack closure integral10.1016/0013-7944(77)90013-3 ↗
33. Krueger R. The virtual crack closure technique: history, approach and applications. NASA/CR-2002-211628, ICASE report no. 2002-10; 2002.
34. Delamination fatigue
35. Mixed-mode delamination of multidirectional carbon fiber/epoxy laminates10.1080/10759419808945903 ↗
36. A fractographic analysis of delamination within multidirectional carbon/epoxy laminates10.1016/0266-3538(95)00099-2 ↗