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% SLFFEA example "b1" (eight-noded linear brick element) - VALIDATED!
%
% Displacements =>
%
% Node#: 0: -0.086324, -0.00055514, 0.121079
% Node#: 1: 0.0952793, -0.00331153, 0.114235
% Node#: 2: 0.0727445, 0.00768949, -0.0394109
% Node#: 3: -0.0774779, -0.0115562, -0.0325665
% Node#: 4: 4.02896e-12, -4.01728e-12, 0.0713128
% Node#: 5: 8.22274e-12, 2.78523e-12, 0.0734239
% Node#: 6: 0.0439568, 8.17943e-12, 0.00211102
% Node#: 7: -0.0397348, -1.15991e-11, 6.718e-12
%
% Note: the smaller order solutions are zeros
%
<Node>
0 % Global object number
3 0 0 0 % Nodal coordinates
<Node>
1 % Global object number
3 0 0 1 % Nodal coordinates
<Node>
2 % Global object number
3 1 0 1 % Nodal coordinates
<Node>
3 % Global object number
3 1 0 0 % Nodal coordinates
<Node>
4 % Global object number
3 0 1 0 % Nodal coordinates
<Node>
5 % Global object number
3 0 1 1 % Nodal coordinates
<Node>
6 % Global object number
3 1 1 1 % Nodal coordinates
<Node>
7 % Global object number
3 1 1 0 % Nodal coordinates
<END> % End of nodes
<MaterialLinearElasticity>
0 % Global material number
E: 3000000 % E
A: 0 % A
I: 0 % I
nu: 0.29 % nu
h: 1
RhoC: 1
END: % End of material definition
<END> % End of materials
<Element3DC0LinearHexahedronStrain>
0 % Global object number
0 % Node 1 ID
1 % Node 2 ID
2 % Node 3 ID
3 % Node 4 ID
4 % Node 5 ID
5 % Node 6 ID
6 % Node 7 ID
7 % Node 8 ID
0 % Material ID
<END> % End of elements
<LoadNode>
0 % Global load number
0 % GN of the element on which the load acts
0 % Point number within the element
3 0 0 10000 % Force vector
<LoadNode>
1 % Global load number
0 % GN of the element on which the load acts
1 % Point number within the element
3 10000 0 0 % Force vector
<LoadNode>
2 % Global load number
0 % GN of the element on which the load acts
2 % Point number within the element
3 0 0 -10000 % Force vector
<LoadNode>
3 % Global load number
0 % GN of the element on which the load acts
3 % Point number within the element
3 -10000 0 0 % Force vector
% Essential boundary conditions in form of MFCs are applyed, so that
% the system is fixed and we can solve for displacements. In book the
% MFCs are different than these here.
<LoadBC>
4 % Global load number
0 % GN of element
12 % DOF# in element
1 0 % rhs of MFC
<LoadBC>
5 % Global load number
0 % GN of element
13 % DOF# in element
1 0 % rhs of MFC
<LoadBC>
6 % Global load number
0 % GN of element
15 % DOF# in element
1 0 % rhs of MFC
<LoadBC>
7 % Global load number
0 % GN of element
16 % DOF# in element
1 0 % rhs of MFC
<LoadBC>
8 % Global load number
0 % GN of element
19 % DOF# in element
1 0 % rhs of MFC
<LoadBC>
9 % Global load number
0 % GN of element
22 % DOF# in element
1 0 % rhs of MFC
<LoadBC>
10 % Global load number
0 % GN of element
23 % DOF# in element
1 0 % rhs of MFC
<END> % End of loads
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