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Composite Materials Research Progress

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An Experimental and Analytical Study of Unidirectional Carbon Fiber… 153<br />

For fiber element:<br />

For matrix element<br />

U i+<br />

1,<br />

j −U<br />

i,<br />

j<br />

σ i,<br />

j = E f<br />

(16a)<br />

X<br />

U i+<br />

1,<br />

j −U<br />

i,<br />

j<br />

σ i,<br />

j = Em<br />

(16b)<br />

X<br />

The strain and stress of composites were calculated from average stress of all elements.<br />

c<br />

n m n m<br />

1 ⎡<br />

⎤<br />

= ×<br />

( )<br />

( ) ⎢∑∑σ<br />

2i+<br />

1,<br />

j 1−<br />

V f + ∑∑σ<br />

2i,<br />

jV<br />

f<br />

2N<br />

+ 1 M<br />

⎥<br />

⎣ i−0<br />

1 1 1 ⎦<br />

σ (17)<br />

Strength of Fiber Element and the Failure Criterion<br />

VKΔt<br />

ε c =<br />

(18)<br />

L<br />

Strength assignment to the fiber elements<br />

In simulating, the strength of the fiber elements should be predetermined. According to<br />

the Weibull statistical constitutive model the strength of the fiber follow Equation (4). If we<br />

assume L in Equation (4) equal to mesh length Δx, here σΔx can be obtained from the scale<br />

parameter σ0 at experimental length Lo. n×m random array ηi,j, equally distributed in the<br />

range of (0,1), are produced by the computer, and we let<br />

η<br />

i,<br />

j<br />

β<br />

⎡ Δx<br />

⎛ S ⎤<br />

i,<br />

j ⎞<br />

= P ( Δx,<br />

S ) = ⎢−<br />

⎜<br />

⎟<br />

i,<br />

j exp<br />

⎥<br />

(19)<br />

⎢ L0<br />

⎣ ⎝ σ 0 ⎠ ⎥<br />

⎦<br />

From the Equation (19), we can get the strength of fiber element<br />

The failure criterion<br />

The failure criterion of fiber is<br />

i,<br />

j ≥ S i,<br />

j<br />

1<br />

i,<br />

j<br />

⎡ L0<br />

= − ln j σ<br />

⎤ β<br />

( ηi,<br />

) 0<br />

S ⎢ ⎥<br />

(20)<br />

⎣ Δx<br />

⎦<br />

σ fiber element broken (21a)

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