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