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Mode I delamination

Historically, most attention has been devoted to mode I delamination growth to assess defects critically, as the first-generation composite systems exhibited low mode I fracture toughness when subjected to interlaminar normal stresses. The... [Pg.76]

Hu, X.Z. and Mai, Y.W. (1993). Mode I delamination and fiber bridging in carbon fiber expoxy composites with and without PVAL coating. Composites Sci. Technol. 46, 147-156. [Pg.88]

The mode I delamination fracture toughness is measured on flat coupons using the Double Cantilever Beam (DCB) test method. The test method utilizes a unidirectional rectangular composite specimen of uniform thickness with nonadhesive insert (as a delamination initiator) at the midplane. This test method is currently in the process of standardization by ASTM. [Pg.415]

Cross-ply laminates. Mode I delamination fracture. Composite, R-curve. [Pg.433]

Figure 8. Computer simulation of mode I delamination of z-pinned laminated composites. Solid lines represent the simulation results and dots represent the experimental data [7]. Figure 8. Computer simulation of mode I delamination of z-pinned laminated composites. Solid lines represent the simulation results and dots represent the experimental data [7].
Theoretical model of mode I delamination of z-pinned DCB has been developed to study the bridging mechanism of z-pin reinforcement. The numerical results show that the fracture load for delamination in the z-pinned DCB is greatly dependant on the fnctional pull-out force Pf. However, since the deformation of the z-pin is relatively small compared to sliding distance, the effects of debonding force and debonding length on the fracture resistance of the DCB are... [Pg.501]

ISO 15.024. Determination of Mode I delamination resistance of unidirectional fibre-reinforced polymer laminates using the double cantilever beam. [Pg.425]

Stelzer S, Brunner AJ, Argiielles A, Murphy N, Cano GM, Pinter G. Mode I delamination fatigue crack growth in unidirectional fiber reinforced composites results from ESIS TC4 round-rohins. Eng Fract Mech 2013 116 92-107. http //dx.doi.org/10.1016/ j. engfracmech.2013.12.002. [Pg.222]

Walker L, Hu XZ. Mode I delamination behavior of short fibre reinforced carbon fibre/ epoxy composites following environmental conditioning. Compos Sci Technol 2003 63 531-7. http //dx.doi.org/10.1016/S0266-3538(02)00224-5. [Pg.223]

Brunner AJ, Blackman BRK, Davies P. Mode I delamination [Chapter 4.1], In Moore DR, Pavan A, Williams JG, editors. Fracmre mechanics test methods for polymers, adhesives and composites. Elsevier 2001. pp. 271—305. http //dx.doi.org/ 10.1016/31566-1369(01)80038-8. [Pg.224]

Hojo M, Matsuda S, Tanaka M, Ochiai S, Murakami S. Mode I delamination fatigue properties of interlayer-toughened CE/epoxy laminates. Compos Sci Technol 2006a 66 665—75. http //dx.doi.Org/10.1016/j.compscitech.2005.07.038. [Pg.225]

Walker L, Hu XZ (2003) Mode I delamination behaviour of shwt fibre reinfOTced carlxm fibre/ epoxy composites following environmental conditimiing. Cranpos Sd Technol 63 (3-4) 531-537... [Pg.144]

Chai, H., The characterization of mode I delamination failure in non-woven, multidirectional laminates. Composites, 14(4), 277-290 (1984). [Pg.440]

See other pages where Mode I delamination is mentioned: [Pg.345]    [Pg.433]    [Pg.491]    [Pg.492]    [Pg.492]    [Pg.498]    [Pg.501]    [Pg.504]    [Pg.514]    [Pg.2322]    [Pg.571]    [Pg.204]    [Pg.206]    [Pg.214]    [Pg.214]    [Pg.215]    [Pg.217]    [Pg.227]    [Pg.347]    [Pg.132]    [Pg.394]   
See also in sourсe #XX -- [ Pg.491 ]



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