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📄 hexa2.fem

📁 DTMK软件开发包,此为开源软件,是一款很好的医学图像开发资源.
💻 FEM
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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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