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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

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