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Journal of Mechanics of Materials and Structures vol. 5 (2010 ... - MSP

Journal of Mechanics of Materials and Structures vol. 5 (2010 ... - MSP

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PLANAR BEAMS: MIXED VARIATIONAL DERIVATION AND FE SOLUTION 789<br />

effects we consider a beam analogous to the one introduced at the beginning <strong>of</strong> Section 6.2 in which we<br />

set l = 2.5 mm. The results are reported in Figures 4, 5, <strong>and</strong> 6. We can appreciate the following:<br />

u [mm x 10 −4 ]<br />

• Far from the boundary, it is possible to recognize the classical beam solution: constant shear stress<br />

τ(x), linear axial stress σx(x), quadratic horizontal displacement u(x), <strong>and</strong> cubic transverse displacement<br />

v(x).<br />

• As expected, boundary effects decay as damped harmonic functions.<br />

• The local effects decay very rapidly, so that only the first oscillation is significant. This result is<br />

consistent with the other models capable <strong>of</strong> capturing these kind <strong>of</strong> boundary effects.<br />

2<br />

1.5<br />

1<br />

0.5<br />

0<br />

−0.5<br />

−1<br />

−1.5<br />

u 2 , u 3<br />

u 4 , u 5<br />

−2<br />

0 0.5 1 1.5 2 2.5<br />

x [mm]<br />

u 1<br />

u 2<br />

u 3<br />

u 4<br />

u 5<br />

u 6<br />

v [mm x 10 −4 ]<br />

0<br />

−2<br />

−4<br />

−6<br />

v 1 , v 9<br />

v 1<br />

v 2<br />

v 3<br />

v 4<br />

v 5<br />

v 6<br />

v 7<br />

v 8<br />

v 9<br />

v 3 , v 4 , v 6 , v 7<br />

v 2 , v 5 , v 8<br />

0 0.5 1 1.5 2 2.5<br />

x [mm]<br />

Figure 4. Axial displacements û (left) <strong>and</strong> transverse displacements ˆv (right) as functions<br />

<strong>of</strong> x for a three-layer homogeneous cantilever, clamped at x = 0, loaded at x = 2.5<br />

by a quadratic shear distribution, <strong>and</strong> modeled with 64 elements.<br />

σ x [MPa]<br />

15<br />

10<br />

5<br />

0<br />

−5<br />

−10<br />

−15<br />

s x1<br />

s x2<br />

s x3<br />

s x4<br />

s x5<br />

s x6<br />

0 0.5 1 1.5 2 2.5<br />

x [mm]<br />

Figure 5. Axial stress ˆσx(x) <strong>of</strong> a three-layer homogeneous cantilever, clamped at x = 0,<br />

loaded at x = 2.5 by a quadratic shear distribution, <strong>and</strong> modeled with 64 elements.

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