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The Finite Element Method for the Analysis of Non-Linear and ...

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Example<br />

<strong>The</strong>re<strong>for</strong>e, we ultimately have:<br />

∂ t x i<br />

∂ 0 x j<br />

=<br />

<strong>The</strong> nodal coordinates at time t are:<br />

4∑<br />

k=1<br />

( ) ∂Nk t x k<br />

∂ 0 i (5)<br />

x j<br />

( t x 1<br />

1<br />

, t x 1 2) = (2 + 4t, 2) ( t x 2 1, t x 2 2) = (4t, 2)<br />

( t x 3 1, t x 3 2) = (0, 0) ( t x 4 1, t x 4 2) = (2, 0)<br />

(6)<br />

By substituting (4), (5) <strong>and</strong> (6) into Eqn (2) we obtain:<br />

[ ]<br />

t 1 2t<br />

0X =<br />

0 1<br />

From Lecture 4 we know that <strong>the</strong> Green-Langrange strain tensor will <strong>the</strong>n be:<br />

t<br />

0ɛ = 1 2 (t 0X T t 0X − I) ⇒<br />

[ ]<br />

t 0 t<br />

0ɛ =<br />

t 2t 2<br />

Institute <strong>of</strong> Structural Engineering <strong>Method</strong> <strong>of</strong> <strong>Finite</strong> <strong>Element</strong>s II 13

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