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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Special Considerations-Geometric Stiffness<br />
Beam <strong>Element</strong><br />
In <strong>the</strong> case <strong>of</strong> a beam element with bending properties in which <strong>the</strong> de<strong>for</strong>med<br />
shape is assumed to be a cubic function due to <strong>the</strong> rotations φ i <strong>and</strong> φ j at <strong>the</strong><br />
ends, additional moments M i <strong>and</strong> M j are developed. <strong>The</strong> <strong>for</strong>ce-displacement<br />
relationship is given by <strong>the</strong> following equation:<br />
⎡<br />
⎢<br />
⎣<br />
F i<br />
M i<br />
F j<br />
M j<br />
⎤<br />
⎥<br />
⎦ =<br />
T<br />
30L<br />
⎡<br />
⎢<br />
⎣<br />
⎤<br />
36 3L −36 3L<br />
3L 4L 2 −3L −L 2<br />
⎥<br />
−36 −3L 36 −3L ⎦<br />
3L −L 2 −3L 4L 2<br />
⎡<br />
⎢<br />
⎣<br />
v i<br />
φ i<br />
v j<br />
φ j<br />
⎤<br />
⎥<br />
⎦<br />
or FG = KGv<br />
<strong>The</strong> well-known elastic <strong>for</strong>ce de<strong>for</strong>mation relationship, <strong>for</strong> a prismatic beam<br />
without shearing de<strong>for</strong>mations, is<br />
⎡ ⎤ ⎡<br />
⎤ ⎡ ⎤<br />
F i<br />
12 6L −12 6L v i<br />
⎢ M i<br />
⎥<br />
⎣ F j<br />
⎦ = EI<br />
⎢ 6L 4L 2 −6L −2L 2<br />
⎥ ⎢ φ i<br />
⎥<br />
L 3 ⎣ −12 −6L 12 −6L ⎦ ⎣ v j<br />
⎦ or FE = KEv<br />
M j<br />
−6L −2L 2 −6L 4L 2 φ j<br />
<strong>The</strong>re<strong>for</strong>e, <strong>the</strong> total <strong>for</strong>ces acting on <strong>the</strong> beam element will be:<br />
F T = F E + F G = [K E + K G]v = K T v<br />
Institute <strong>of</strong> Structural Engineering <strong>Method</strong> <strong>of</strong> <strong>Finite</strong> <strong>Element</strong>s II 52