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Composite Materials Research Progress

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Multi-scale Analysis of Fiber-Reinforced <strong>Composite</strong> Parts… 19<br />

obviously directly related to the discrepancies previously underlined in subsection 2.5 where<br />

the question of comparing the homogenization relations of the two scale transition methods<br />

presented in this paper, was investigated.<br />

Table 3. Pseudomacroscopic elastic moduli and stiffness tensor components assumed for<br />

the epoxy matrix of the composite plies at ΔC 0<br />

I = % and T I = 300 K, according to<br />

(Herakovich, 1998).<br />

Elastic moduli<br />

Stiffness tensor<br />

components<br />

m<br />

1<br />

m<br />

Y 2 [GPa]<br />

m<br />

ν 12 [1]<br />

m<br />

G 12 [GPa]<br />

m<br />

23<br />

5.35 5.35 0.350 1.98 1.98<br />

Y [GPa]<br />

G [GPa]<br />

m<br />

11<br />

m<br />

L 22 [GPa]<br />

m<br />

L 12 [GPa]<br />

m<br />

L 44 [GPa]<br />

m<br />

L 55 [GPa]<br />

8.62 8.62 4.66 1.98 1.98<br />

L [GPa]<br />

Table 4. Pseudomacroscopic elastic moduli and stiffness tensor components identified<br />

for the carbon fiber reinforcing the composite plies at ΔC 0<br />

I = % and T I = 300 K,<br />

according to either Mori-Tanaka estimates, or Eshelby-Kröner self-consistent model.<br />

Comparison with the corresponding properties exhibited in practice by typical highstrength<br />

carbon fibers, according to (Herakovich, 1998).<br />

Elastic moduli<br />

r<br />

Y 1 [GPa]<br />

r<br />

Y 2 [GPa]<br />

r<br />

ν 12 [1]<br />

r<br />

G 23 [GPa]<br />

r<br />

G 12 [GPa]<br />

Mori-Tanaka estimate 213.1 13.7 0.27 4.1 22.7<br />

Eshelby-Kröner model 213.2 13.3 0.27 4.0 12.1<br />

Typical expected<br />

properties<br />

Stiffness tensor<br />

components<br />

232 15 0.279 5.0 15<br />

r<br />

L 11[GPa]<br />

r<br />

L 22 [GPa]<br />

r<br />

L 12 [GPa]<br />

r<br />

L 44 [GPa]<br />

r<br />

L 55 [GPa]<br />

Mori-Tanaka estimate 219.2 24.9 11.2 4.1 22.7<br />

Eshelby-Kröner model 219.2 23.9 10.8 4.0 12.1<br />

Typical expected<br />

properties<br />

236.7 20.1 8.4 5.02 15<br />

3.3.2. Determination of AS4/3501-6 Matrix Coefficients of Moisture Expansion<br />

Macroscopic values of the Coefficients of Moisture Expansion are sometimes available,<br />

contrary to the corresponding pure epoxy resin CME. Simulations were performed in the cas<br />

e of an AS4/3501-6 composite, with a reinforcing fiber volume fraction v r =0.60. The<br />

calculations were achieved using the elastic properties given in Table 5, and the macroscopic<br />

coefficients of moisture expansion listed in Table 6. The same table summarizes the results<br />

obtained with both inverse Eshelby-Kröner self-consistent model (21) and Mori-Tanaka

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