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Rock Mechanics.pdf - Mining and Blasting

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THE DISTINCT ELEMENT METHOD<br />

Equilibrium at any node requires that the applied external force at the node be in balance<br />

with the resultant internal equivalent nodal force. Suppose the internal equivalent<br />

nodal force vector for elements a <strong>and</strong> b is given by<br />

[q a ] T = q a x1 qa y1 qa x2 qa y2 qa x3 qa <br />

y3<br />

[q b ] T = q b x2 qb y2 qb x4 qb y4 qb x3 qb <br />

y3<br />

The nodal equilibrium condition requires<br />

for node 1: rx1 = q a x1 , ry1 = q a y1<br />

for node 2: rx2 = q a x2 + qb x2 , ry2 = q a y2 + qb y2<br />

with similar conditions for the other nodes. The external force–nodal displacement<br />

equation for the assembly then becomes<br />

⎡ ⎤ ⎡<br />

rx1<br />

⎢ ry1 ⎥ K<br />

⎢ ⎥ ⎢<br />

⎢ rx2 ⎥ ⎢<br />

⎢ ⎥ ⎢<br />

⎢ ry2 ⎥ ⎢<br />

⎢ ⎥ ⎢<br />

⎢ rx3 ⎥ = ⎢<br />

⎢ ⎥ ⎢<br />

⎢ ry3 ⎥ ⎢<br />

⎢ ⎥ ⎢<br />

⎣ rx4 ⎦ ⎣<br />

a 0 0<br />

0 0<br />

------------<br />

K a + K b<br />

------------<br />

0 0 K b<br />

0 0 --------- ⎤ ⎡ ⎤ ⎡ ⎤<br />

ux1 fx1<br />

⎥ ⎢<br />

⎥ ⎢ u ⎥ ⎢<br />

y1 fy1 ⎥<br />

⎥ ⎢ ⎥<br />

⎥ ⎢ ux2 ⎥ ⎢ fx2 ⎥<br />

⎥ ⎢ ⎥ ⎢ ⎥<br />

⎥ ⎢<br />

⎥ ⎢ u ⎥ ⎢<br />

y2 fy2 ⎥<br />

⎥<br />

⎥ ⎢ ux3 ⎥ + ⎢ ⎥<br />

⎢ fx3 ⎥<br />

⎥ ⎢ ⎥ ⎢ ⎥<br />

⎥ ⎢<br />

⎦ ⎢ u ⎥ ⎢<br />

y3 fy3 ⎥<br />

⎥ ⎢ ⎥<br />

⎣ ux4 ⎦ ⎣ fx4 ⎦<br />

ry4<br />

----------<br />

where appropriate elements of the stiffness matrices [K a ] <strong>and</strong> [K b ] are added at the<br />

common nodes. Thus assembly of the global stiffness matrix [K] proceeds simply by<br />

taking account of the connectivity of the various elements, to yield the global equation<br />

for the assembly<br />

u y4<br />

fy4<br />

[K][u g ] = [r g ] − [f g ] (6.44)<br />

Solution of the global equation 6.44 returns the vector [u g ] of nodal displacements.<br />

The state of stress in each element can then be calculated directly from the appropriate<br />

nodal displacements, using equation 6.41.<br />

In practice, special attention is required to render [K] non-singular, <strong>and</strong> account<br />

must be taken of any applied tractions on the edges of elements. Also, most finite element<br />

codes used in design practice are based on curvilinear quadrilateral elements <strong>and</strong><br />

higher-order displacement variation with respect to the element intrinsic co-ordinates.<br />

For example, a quadratic isoparametric formulation imposes quadratic variation of<br />

displacements <strong>and</strong> quadratic description of element shape. Apart from some added<br />

complexity in the evaluation of the element stiffness matrix <strong>and</strong> the initial load vector,<br />

the solution procedure is essentially identical to that described here.<br />

6.7 The distinct element method<br />

Both the boundary element method <strong>and</strong> the finite element method are used extensively<br />

for analysis of underground excavation design problems. Both methods can<br />

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