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

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Truss <strong>and</strong> Cable <strong>Element</strong>s - Example<br />

In order to derive <strong>the</strong> nonlinear part <strong>of</strong> <strong>the</strong> stiffness matrix we first need to evaluate <strong>the</strong><br />

Piola-Kirchh<strong>of</strong>f stress. We know that <strong>the</strong> Cauchy stress at time t is equal to t t P<br />

τ =<br />

t A ,<br />

directed along <strong>the</strong> axis <strong>of</strong> <strong>the</strong> element at time t. Using <strong>the</strong> rotational matrix we can<br />

rotate <strong>the</strong> stress tensor from <strong>the</strong> element axis system to <strong>the</strong> original reference system<br />

( t x 1 , t x 2 ). Denoting <strong>the</strong> rotated tensor as t ¯τ we have:<br />

t ¯τ = R<br />

[ t τ 0<br />

0 0<br />

]<br />

[<br />

R T cosθ −sinθ<br />

, R =<br />

sinθ cosθ<br />

<strong>The</strong>n, from Lecture 4 we know that <strong>the</strong> Piola-Kirchh<strong>of</strong>f stress is given as:<br />

t<br />

0 [<br />

0 S = ρ<br />

t<br />

0<br />

t t X t ¯τ 0 t X T τ 0<br />

or R<br />

ρ<br />

0 0<br />

]<br />

R T =<br />

]<br />

t ρ t<br />

0 0<br />

ρ<br />

X t 0 S t 0 XT (10)<br />

where <strong>the</strong> de<strong>for</strong>mation gradient, t 0X, can be obtained as <strong>the</strong> product <strong>of</strong> a rotational <strong>and</strong><br />

a stretch component as t 0X = RU. For this example <strong>the</strong> stretch matrix is obviously<br />

(elongation along x):<br />

⎡<br />

⎤<br />

⎡<br />

0 L + ∆L<br />

U = ⎣ 0 0 ⎦<br />

L<br />

⇒ U −1 = ⎣<br />

0 1<br />

0 L<br />

0 L + ∆L 0<br />

0 1<br />

⎤<br />

⎦<br />

Institute <strong>of</strong> Structural Engineering <strong>Method</strong> <strong>of</strong> <strong>Finite</strong> <strong>Element</strong>s II 23

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