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Interlaminar fracture test

Fig. 3.30. Schematic illustrations of Mode I interlaminar fracture test specimens (a) DCB specimen (b)... Fig. 3.30. Schematic illustrations of Mode I interlaminar fracture test specimens (a) DCB specimen (b)...
The pure mode II interlaminar fracture testing can be performed using both the end notched flexure (ENF) specimen (Russell and Street, 1984, 1985) and the end loaded split (ELS) specimen (Corleto and Bradley, 1987 Prel et al.. 1989) (Fig 3.32). [Pg.81]

Fig. 3.33. CLS specimen for mixed mode interlaminar fracture tests. Fig. 3.33. CLS specimen for mixed mode interlaminar fracture tests.
Davies, P. and Roulin. A. (1989). A standard for interlaminar fracture testing of composites. In Proc. ECCM 3, Developments in the Science and Technology of Composite Materials. (A.R. Bunsell, P. Lamicq and A. Massiah eds.), Elsevier Appl. Sci., London, pp. 419-424. [Pg.87]

Davies, P. Kausch, H.H., Williams, J.G. and 29 other researchers (1992). Round-robin interlaminar fracture testing of carbon fiber reinforced epoxy and PEEK composites. Composites Sci. Technol. 43, 129-136. [Pg.87]

F.iiropean Structural Integrity Society. Polymers and Composites Task Group, Protocols for Interlaminar Fracture Testing of Composites." draft by P. Davies, May 1992. [Pg.586]

Protocol for interlaminar fracture testing of composites (mode I DCB - ISO 15 024 and mode II ELS - ESIS TC4)... [Pg.461]

O Brien, T.K. and Martin, R.H. (1992). Results of ASTM round robin testing for mode I interlaminar fracture toughness of composite materials, NASA TM 104222. [Pg.90]

Figure 11. Sketch of the specimen and test configuration to detect EE and AE from the interlaminar fracture of graphite/epoxy composites. Figure 11. Sketch of the specimen and test configuration to detect EE and AE from the interlaminar fracture of graphite/epoxy composites.
ISO, Standard test method for mode I interlaminar fracture toughness, G/c, of unidirectional fibre-reinforced polymer matrix Composites. ISO 15024 2001. Blackman, B.R.K., H. Hadavinia, A.J. Kinloch, M. Paraschi and J.G, Williams, The calculation of adhesive fracture energies in mode I revisiting the tapered double cantilever beam (TDCB) test. Engineering Fracture Mechanics 2003. 70 p. 233-248. BSI, Determination of the mode I adhesive fracture energy, Gic, of structural adhesives using the double cantilever beam (DCB) and tapered double cantilever beam (TDCB) specimens. 2001. BS 7991. [Pg.304]

Davies, P., G.D. Sims, B.R.K. Blackman, A.J. Brunner, K. Kageyama, M. Hojo, K. Tanaka, G.B. Murri, C.Q. Rousseau, B. Gieseke, and R. Martin, Comparison of test configurations for determination of mode II interlaminar fracture toughness results from international collaborative test programme. Plastics, Rubber and Composites, 1999. 28(9) p. 432-437. [Pg.304]

Blackman, B.R.K. and J.G. Williams. On the mode II testing of carbon-fibre polymer composites, in ECFI2 Fracture from Defects. 1998. Sheffield, UK EMAS publishing, Hashemi, S., A.J. Kinloch, and J.G. Williams, The analysis of interlaminar fracture in uniaxial fibre-polymer composites. Proceeding of the Royal Society London, 1990. A427 p. 173-199. [Pg.304]

Fig. 5. Relationship between load and crack opening Fig. 6. Relationship between normalized crack displacement for mode I interlaminar fracture tough- length and compliance for DCB specimen in ness tests inT300/EpoxyH and Altex/EpoxyH lami- T300/EpoxyH laminates in TTK-LN -nates in 77K-LN,. Fig. 5. Relationship between load and crack opening Fig. 6. Relationship between normalized crack displacement for mode I interlaminar fracture tough- length and compliance for DCB specimen in ness tests inT300/EpoxyH and Altex/EpoxyH lami- T300/EpoxyH laminates in TTK-LN -nates in 77K-LN,.
Fig. 10. Effects of fiber type (T300 and Altex) and test environment (RT-air and 77K-LN on the relation between mode II interlaminar fracture toughness and increment of crack length in fiber/ poxyH laminates. Fig. 10. Effects of fiber type (T300 and Altex) and test environment (RT-air and 77K-LN on the relation between mode II interlaminar fracture toughness and increment of crack length in fiber/ poxyH laminates.
ISO 15024. (2001) Standard test method for mode I interlaminar fracture toughness, G/c, of unidirectional fibre-reinforced polymer matrix composites. [Pg.488]

A summary of quasi-static delamination test methods for continuous-fibre, unidirectional FRP composites is given in Table 8.1. For mode 1, several standard test methods exist, namely, JIS K7086 ( Testing methods for interlaminar fracture toughness of carbon fibre reinforced plastics , 1993) this also includes a quasi-static mode 11 standard test, ASTM... [Pg.196]

Shindo Y, Takahashi S, Takeda T, NaritaF, Watanahe. Mixed-mode interlaminar fracture and damage characterization in woven fahric-teinforced glass/epoxy composite laminates at cryogenic temperatures using the finite element and improved test methods. Eng Fract Mech 2008 75 5101-12. http //dx.doi.Org/10.1016/j.engfracmech.2008.07.009. [Pg.228]

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