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Non-local Models of Stiffness and Damping - Michael I Friswell

Non-local Models of Stiffness and Damping - Michael I Friswell

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two major problems with this approach to obtaining the kernel functions. First, a transverse force is applied to<br />

the node at x = L /2, <strong>and</strong> the adjacent nodes are fixed. This means there is a significant deformation within the<br />

element near this forced node that is unlikely to be captured accurately by the shape functions with the element.<br />

In practice this means that the estimated kernel function is unlikely to be accurate close to x = L /2. Second,<br />

normalization <strong>of</strong> the kernel function is difficult, because the <strong>local</strong> stiffness <strong>of</strong> the forced degree <strong>of</strong> freedom<br />

changes with mesh density, the imposed displacement on the neutral axis is not a delta function, <strong>and</strong> also<br />

because the inaccuracies <strong>of</strong> the deformation <strong>and</strong> constraining forces close to x = L /2.<br />

Figure 5 – A typical 2D finite element mesh <strong>of</strong> the foundation. There are 20 elements along the beam axis <strong>and</strong> 4 across the<br />

thickness <strong>of</strong> the foundation. All elements model the foundation.<br />

Figure 6 shows the kernel function obtained for three different mesh densities <strong>and</strong> a foundation length <strong>of</strong> 1 m <strong>and</strong><br />

a foundation thickness <strong>of</strong> 0.2 m. The elements used were 4-noded rectangular elements (Dawe [11], p. 325). A<br />

plane stress element was used, although the results are very similar for plane strain. The thickness <strong>and</strong> modulus<br />

<strong>of</strong> the foundation material merely changes the normalization <strong>of</strong> the kernel. Poisson’s ratio was taken as 0.3. The<br />

number <strong>of</strong> elements in each direction is chosen so that the elements are square. The results are shown on a semilog<br />

plot, where the kernel is positive for x −ξ< 0.175 , <strong>and</strong> negative for x −ξ> 0.175 . Clearly the estimated<br />

kernel functions are almost identical along most <strong>of</strong> the beam length. For x −ξ close to zero there are differences<br />

in the estimated kernel for the reasons discussed above. Near the end <strong>of</strong> the foundation, x − ξ ≈ 1 , there are also<br />

some differences, however the estimated kernel is unlikely to be accurate close to this location, as shown by the<br />

increase in the kernel for all element mesh densities for x>0.95.<br />

Figure 6 – The estimated kernel function for three different mesh densities.<br />

Figure 6 shows two regions where the plot is approximately linear, namely 0.05 < x −ξ < 0.15 <strong>and</strong><br />

0.35 < x −ξ < 0.85 , showing that the kernel may be approximated using the sum <strong>of</strong> two exponential functions.<br />

Neglecting the estimated kernel for x − ξ < 0.05 <strong>and</strong> x −ξ> 0.92 for the 8000 element example, <strong>and</strong> curve

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