* -------1st PART (MATERIAL PROP., GEOMETRY, BOUNDARY CONDITIONS)------

* POISSONS RATIO, YOUNGS MOD, #PLANES, COEFF FRICTION, BACKGROUND DEFORMATION
.25 7.E10 2 0.6 displacement gradient
* Background deformation tensor
0 0 0 0 -.00001 0 0 0 0

 

* for each element or plane specify the
* REFERENCE:XO YO ZO, DIMEN.:STK DIP, #SUB-ELEMS:STK DIP GEOM:STK DIP
50. 59. .0 136. 15. 3 2 48. 90.
122. 180. .0 54. 15. 1 2 37. 90.

 

* for each plane (at each fixed distance along strike, going up-dip):
* PLN, SUB-ELEM code BC-shear(STK) BC2-shear(DIP) BC3-normal
* 1 (STK,DIP)
1 1 10 -270. 0.0 0.0
1 2 10 -270. 0.0 0.0
2 1 10 -270. 0.0 0.0
2 2 10 -270. 0.0 0.0
3 1 10 -270. 0.0 0.0
3 2 10 -270. 0.0 0.0
* 2 (STK,DIP)
1 1 10 -270. 0.0 0.0
1 2 10 -270. 0.0 0.0

 

* --------------2nd PART (OUTPUT CONTROL)----------------------------------

* Block #1: Run everything else non-interactively
Not Interactive (alternative is 'Interactive' grid specification)
Plane grid (alternative is 'Volume grid')
Vector output (alternative is 'XYZ'--vector output yields both types of output files)
*

* Block #2: Coordinate system for output (global only for volume grids)
planar (in-plane coordinates of gridded plane--must not begin with "g")
*
* Block #3: Output information (each line results in a separate output file)
stress (in global coordinates)
strain (in global coordinates)
gradients of displacement (in global coordinates)
rigid body rotations (about the global X(E),Y(N),Z(up) axes)
orientation of principal strain axes (w.r.t the global X(E),Y(N),Z(up) coordinates)
displacements (in global coordinates)
invariants of the strain field (independent of coordinate system)
failure planes (in global coordinates)
element relative displacements (strike,dip,normal directions of each element's plane)
*
* Block #4: Output file suffix
outB
*
* Block #5: Xo,Yo,Zo (Ref. corner),strike (cw wrt N),dip (0-90),length (strike), width (dip):
0,0,0,90,90,10,5
* Number of grid points in the strike and dip directions:
5,5