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

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Example<br />

In order to define <strong>the</strong> required stresses <strong>and</strong> strains we need to determine <strong>the</strong> de<strong>for</strong>mation<br />

gradient t 0S, which in 2D is written as:<br />

⎡<br />

∂ t x 1 ∂ t ⎤<br />

x 1<br />

t<br />

0 X = ⎢ ∂ 0 x 1 ∂ 0 x 2<br />

⎣ ∂ t x 2 ∂ t ⎥<br />

x 2 ⎦ (2)<br />

∂ 0 x 1 ∂ 0 x 2<br />

<strong>The</strong> coordinates <strong>of</strong> a r<strong>and</strong>om point within <strong>the</strong> element are given as <strong>the</strong> weighted sum <strong>of</strong><br />

<strong>the</strong> nodal coordinates, where <strong>the</strong> weights are <strong>the</strong> shape functions. However, <strong>the</strong> shape<br />

functions are written with respect to <strong>the</strong> r, s system (isoparametric representation) as:<br />

N 1 = 1 4 (1 + r)(1 + s) N 2 = 1 (1 − r)(1 + s)<br />

4<br />

N 3 = 1 4 (1 − r)(1 − s) N 4 = 1 (3)<br />

4 (1 + r)(1 − s)<br />

From <strong>the</strong> given figure however we see that <strong>the</strong> 0 x 1 , 0 x 2 system is related to <strong>the</strong> r, s<br />

system through:<br />

0 x 1 = r + 1<br />

0 x 2 = s + 1 ⇒<br />

N 1 = 1 4 0 x 1 0 x 2 N 2 = 1 4 (2 − 0 x 1 )( 0 x 2 )<br />

(4)<br />

N 3 = 1 4 (2 − 0 x 1 )(2 − 0 x 2 ) N 4 = 1 4 0 x 1 (2 − 0 x 2 )<br />

Institute <strong>of</strong> Structural Engineering <strong>Method</strong> <strong>of</strong> <strong>Finite</strong> <strong>Element</strong>s II 12

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