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Experimental Investigation Of Multiwalled…<br />

Combining Eqs. (1), (6) and (7) gives us the general form for potential energy loss due to matrix<br />

cracking, from state (1) to state (2):<br />

π1-π2=1/2∫v (σ1―σ2): (ε1―ε2) dV (8)<br />

Derivation of the potential energy loss in the case of an elastic body containing frictional sliding and<br />

fiber breakage, in our case due to nanotube pull-out and the fracture of CNTs, proceeds much the same as<br />

before, up until the calculation of the virtual work. For completeness, the potential energy equation for the<br />

second case takes the exact form as its predecessor, Eq. (6), but with accented rather than natural notation:The<br />

difference in the derivation of the energy relations in the hybrid matrix case is the two additional internal virtual<br />

work terms corresponding to the frictional sliding and fiber breakage<br />

IV. CONCLUSIONS<br />

The addition of 1wt% of CNTs to the polymer matrix of glass fiber-epoxy composite laminates<br />

improved their high-cycle fatigue lifetimes significantly. Tensile tests on neat resin (without glass fibers)<br />

specimens showed no effect on the elastic modulus when CNTs were added. However, there was a slight<br />

increase in the strain to failure and corresponding higher toughness relative to the unmodified resin. High<br />

resolution scanning electron microscopy of the neat resin specimens after tensile fracture revealed somewhat<br />

higher surface roughness in the CNT-modified resin. Inspection of the composite specimens tested in fatigue<br />

showed carbon nanotubes that were either pulled out of the resin matrix or fractured, suggesting energyabsorbing<br />

mechanisms that may be responsible for the increase in the fatigue life observed. These include the<br />

creation of a much larger density of nucleation sites for fatigue crack initiation in the epoxy matrix as well as<br />

possible crack bridging by the carbon nanotubes. Both mechanisms can result in a significant increase in crack<br />

energy absorption during fatigue crack initiation, coalescence and propagation, resulting in the observed<br />

increase in the fatigue life when carbon nanotubes are added.<br />

The energy based model presented here takes advantage of the even distribution and random<br />

orientation of the large numbers of CNTs in the polymer matrix and uses this as a basis for establishing a<br />

micrometer-scale representative volume element with homogenized material properties that reflect the<br />

mechanistic behavior of the entire population of CNTs it contains. Energy relations are developed for this<br />

homogenized CNT / epoxy system in parallel with the neat epoxy matrix in order to establish the energetic<br />

differences, or differential energy, in the formation and propagation of cracks within their bodies.This study<br />

shows that the addition of small fractions of carbon nanotubes to glass fiber composites can result in a<br />

significant increase in their fatigue life, making glass fiber composites more useful in applications involving<br />

high-cycle fatigue.<br />

REFERENCES<br />

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1975, 569: 171<br />

[2] Dharan CKH. Fatigue Failure in Graphite Fibre and Glass Fabre- polymer Composites [J]. J. Mater. Sci., 1975, 10: 1 655<br />

[3] Hahn HT, Kim RY. Fatigue Behavior of Composite Laminate [J]. J. Compos. Mater, 1976, 10: 156<br />

[4] Degrieck J, Van Paepegem W. Fatigue Damage Modeling of Fiber-reinforced Composite Materials: Review [J]. Appl.<br />

Mech. Rev., 2001, 54(4): 279<br />

[5] Saghizadeh H, Dharan CKH. Delamination Fracture Toughness of Graphite and Aramid-epoxy Composites [J]. J. Eng. Mater.<br />

Tech.: Trans. ASME, 1986, 108(4): 290<br />

[6] Ren Y, Lil F, Cheng HM, et al. Fatigue Behaviour of Unidirectional Single-walled Carbon Nanotube Reinforced<br />

Epoxy Composite under Tensile Load[J]. Adv. Compos. Lett., 2003, 12(1): 19<br />

[7] Ganguli S, Aglan H. Effect of Loading and Surface Modification of MWCNTs on the Fracture Behavior of Epoxy Nan<br />

composites [ J]. J. Reinforc. Plast. Compos. 2006, 25(2): 175<br />

[8] Grimmer CS, Dharan CKH. High-cycle Fatigue of Hybrid Carbon Nanotube/Glass Fiber/Polymer Composites [J]. J. Mater. Sci.,<br />

2008, 43: 4487<br />

[9] Gojny FH, Wichmann MHG, Fiedler B, et al. Influence of Nano-modification on the Mechanical and Electrical Properties of<br />

Conventional Fibre-reinforced Composites [J]. Compos. A, 2005, 36: 1525<br />

[10] Kim JA, Seong DG, Kang TJ, et al. Effects of Surface Modification on Rheological and Mechanical Properties of<br />

CNT/Epoxy Composites [J]. Carbon, 2006, 44: 1898<br />

[11] Wong M, Paramsothy M, Xu XJ, et al. Physical Interactions at Carbon Nanotube-polymer Interface[J]. Polym.,<br />

2003, 44(25): 7757<br />

[12] Fan Z, Hsiao KT, Advani SG. Experimental Investigation of Dispersion during Flow of Multi-walled Carbon Nanotube/<br />

Polymer Suspension in Fibrous Porous Media [J]. Carbon, 2004, 42: 871<br />

[13] Schadler LS, Giannaris SC, Ajayan PM. Load Transfer in Carbon Nanotube Epoxy Composites [J]. Appl. Phys. Lett.,<br />

1998, 73: 3842<br />

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