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dat input file for DRAGON5
------------------------------------------------------------
* typge, nbfo, node, elem, macr, nreg, z, mac2
9, 0, 5, 10, 1, 5, 0, 1
* index kindex
0 0 1
* eps eps0
1.000000E-05 1.000000E-05
* flux region number per geometry region (mesh)
1, 2, 3, 4, 5
* names of macros
mac
* macro order number per flux region
5*1
elements
* ELEM 1 line segment
1, 0, 5
*
-0.785219, 0.000000, 0.392610, -0.680020
* ELEM 2 line segment
1, 0, 5
*
-0.392610, 0.680020, -0.392610, -0.680020
* ELEM 3 line segment
1, 0, 5
*
-0.392610, -0.680020, 0.785219, -0.000000
* ELEM 4 circle
2, 1, 2
*
0.000000, 0.000000, 0.100000, 0.0
* ELEM 5 circle
2, 2, 3
*
0.000000, 0.000000, 0.450000, 0.0
* ELEM 6 circle
2, 3, 4
*
0.000000, 0.000000, 0.465000, 0.0
* ELEM 7 circle
2, 4, 5
*
0.000000, 0.000000, 0.525000, 0.0
* ELEM 8 line segment
1, 0, 5
*
0.392610, 0.680020, -0.785219, 0.000000
* ELEM 9 line segment
1, 0, 5
*
0.392610, -0.680020, 0.392610, 0.680020
* ELEM 10 line segment
1, 0, 5
*
0.785219, 0.000000, -0.392610, 0.680020
* boundaries conditions: defaul nbbcda allsur
0, 6, 0
* albedo
1.0
* type number of elements
2, 1
* elements
1
* tx, ty, angle
1.177829 0.680020 0.000000
* type number of elements
2, 1
* elements
2
* tx, ty, angle
1.177829 -0.680020 0.000000
* type number of elements
2, 1
* elements
3
* tx, ty, angle
0.000000 1.360040 0.000000
* type number of elements
2, 1
* elements
8
* tx, ty, angle
0.000000 -1.360040 0.000000
* type number of elements
2, 1
* elements
9
* tx, ty, angle
-1.177829 0.680020 0.000000
* type number of elements
2, 1
* elements
10
* tx, ty, angle
-1.177829 -0.680020 0.000000
# 6 - HOLLOW
# 3 - MOX
# 6 - GAP
# 7 - CLADDING
# 8 - COOLANT
* medium number per region
6
3
6
7
8
------------------------------------------------------------
this is the last line generated by conversion
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