Seismic Design of Tunnels - Parsons Brinckerhoff
Seismic Design of Tunnels - Parsons Brinckerhoff
Seismic Design of Tunnels - Parsons Brinckerhoff
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Numerical Analysis<br />
A series <strong>of</strong> computer analyses using finite difference code (FLAC, 1989) is performed<br />
to verify the proposed procedure in the previous section. The mesh and the lining-ground<br />
system used in these analyses are shown in Figure 17. The assumptions made for these<br />
analyses include the following:<br />
• Plane strain conditions are assumed.<br />
• <strong>Seismic</strong> shear wave loading is simulated by pure shear conditions with shear stresses<br />
applied at far external boundaries.<br />
• Taking advantage <strong>of</strong> the anti-symmetric loading conditions, only one quarter <strong>of</strong> the<br />
entire lining/ground system is analyzed. Rollers are provided at planes <strong>of</strong> antisymmetry.<br />
• Lining is modeled by a series <strong>of</strong> continuous flexural beam elements <strong>of</strong> linear elasticity.<br />
• Ground (medium) is modeled as linear elastic material.<br />
• No-slip condition along the lining-ground interface is assumed.<br />
A total <strong>of</strong> 13 analyses are performed. In order to cover a wide range <strong>of</strong> possible<br />
effects <strong>of</strong> lining-ground interaction, the parameters for lining and ground are varied.<br />
Following is a list <strong>of</strong> the range <strong>of</strong> the variations:<br />
Range <strong>of</strong> E m = from 325 ksf to 72000 ksf<br />
n m = 0.25 and 0.333<br />
E l /(1-n l<br />
2) = 518400 ksf and 662400 ksf<br />
Range <strong>of</strong> t = from 0.5 feet to 2.0 feet<br />
The resulting flexibility ratios, F, and compressibility ratios, C, are tabulated in Table 2.<br />
To make the level <strong>of</strong> seismic loading within a reasonable range, the boundary shear<br />
stresses (t max ) are made to result in the maximum free-field shear strains (g max ) in the<br />
range between 0.001 and 0.008.<br />
Results and Recommendations<br />
Maximum Bending Moment, M max . The resulting maximum bending moments are first<br />
calculated for each <strong>of</strong> the 13 cases by using the full-slip closed form solution, Equation 4-<br />
9. These values are then compared to those obtained from the no-slip finite difference<br />
analysis. A plot <strong>of</strong> comparison in terms <strong>of</strong> dimensionless bending moment between the<br />
two is shown in Figure 18. As expected, the full-slip interface assumption results in higher<br />
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