Non-local Models of Stiffness and Damping - Michael I Friswell
Non-local Models of Stiffness and Damping - Michael I Friswell
Non-local Models of Stiffness and Damping - Michael I Friswell
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Figure 2 – A beam with a partial non-<strong>local</strong> foundation.<br />
3. A NUMERICAL EXAMPLE<br />
A simply supported uniform beam <strong>of</strong> length L = 6.096m rests on a uniform non-<strong>local</strong> elastic foundation is<br />
considered, as shown in Figure 1 with x 0 = 0 <strong>and</strong> x2<br />
= L (that is the foundation supports the whole beam). This<br />
example was also analyzed by Lai et al. [8] <strong>and</strong> Thambiratnam <strong>and</strong> Zhuge [9]. The beam has Young’s modulus<br />
-3 4<br />
24.82GPa, second moment <strong>of</strong> area 1.439 × 10 m <strong>and</strong> mass per unit length 446.3kg/m . The stiffness <strong>of</strong> the<br />
foundation is 16.55MNm -2 . Using the finite element method, the first four natural frequencies <strong>of</strong> free vibration<br />
were obtained with 6, 8 <strong>and</strong> 10 elements, for different values <strong>of</strong> α for the exponential kernel. The results are<br />
shown in Table 1 together with those from the analytical solution [10], given by<br />
4<br />
EI i π 4 H0<br />
ωi<br />
= + . (12)<br />
ρA<br />
4<br />
L EI<br />
Figure 3 shows the effect <strong>of</strong> varying α on these natural frequencies for the finite element model with 10<br />
elements.<br />
α ( m −1<br />
)<br />
2 2 2 5 10 50 ∞ ∞<br />
N e<br />
6 8 10 10 10 10 10 Analytical<br />
Mode 1 32.137 32.137 32.137 32.758 32.862 32.897 32.898 32.898<br />
Mode 2 55.310 55.287 55.281 56.495 56.728 56.808 56.812 56.808<br />
Mode 3 110.89 110.62 110.54 111.61 111.86 111.95 111.95 111.90<br />
Mode 4 194.85 193.36 192.92 193.74 193.98 194.07 194.08 193.76<br />
Table 1 – Natural frequencies (Hz) <strong>of</strong> vibration <strong>of</strong> a simple beam on a non-<strong>local</strong> elastic foundation with an exponential<br />
kernel. N e is the number <strong>of</strong> elements.<br />
Figure 3 – The variation <strong>of</strong> the first four natural frequencies with α for the fully supported beam <strong>and</strong> an exponential kernel.<br />
The natural frequencies have been normalized using the values at α = ∞ <strong>and</strong> 10 elements were used.