Code: Select all

```
FemTools.setup_working_dir() --> self.working_dir = /tmp/FEMWB/
FemInputWriterCcx --> self.dir_name --> /tmp/FEMWB/
FemInputWriterCcx --> self.main_file_name --> Fusion_Mesh.inp
FemInputWriterCcx --> self.file_name --> /tmp/FEMWB//Fusion_Mesh.inp
(' ReferenceShape : ', 'Face', ', ', 'Fusion', ', ', u'Fusion', ' --> ', 'Face5')
(' ReferenceShape : ', 'Face', ', ', 'Fusion', ', ', u'Fusion', ' --> ', 'Face8')
(' ReferenceShape : ', 'Face', ', ', 'Fusion', ', ', u'Fusion', ' --> ', 'Face6')
(' ReferenceShape : ', 'Face', ', ', 'Fusion', ', ', u'Fusion', ' --> ', 'Face10')
len femnodes_ele_table:2983
(' ReferenceShape : ', 'Face', ', ', 'Fusion', ', ', u'Fusion', ' --> ', 'Face9')
len femnodes_ele_table:2983
len node_set: 577
len bit_pattern_dict:1316
('found Faces: ', 252)
('faces: ', [[1322, 2], [1516, 1], [1701, 1], [1727, 1], [1728, 1], [1729, 1], [1733, 3], [1745, 2], [1746, 3], [1751, 3], [1754, 2], [1756, 1], [1757, 4], [1759, 4], [1761, 1], [1762, 1], [1763, 2], [1765, 1], [1773, 2], [1775, 1], [1778, 2], [1779, 2], [1781, 1], [1782, 4], [1786, 3], [1803, 2], [1804, 2], [1805, 2], [1806, 4], [1807, 2], [1809, 3], [1810, 4], [1812, 4], [1813, 3], [1815, 1], [1817, 2], [1821, 4], [1824, 3], [1825, 3], [1826, 2], [1828, 4], [1830, 2], [1834, 1], [1836, 2], [1839, 1], [1840, 3], [1842, 1], [1846, 2], [1847, 4], [1848, 2], [1852, 4], [1854, 1], [1866, 4], [1869, 4], [1875, 3], [1881, 2], [1882, 1], [1883, 2], [1885, 3], [1886, 3], [1888, 3], [1895, 1], [1896, 2], [1897, 2], [1902, 2], [1905, 1], [1914, 2], [1921, 4], [1933, 2], [1935, 2], [1940, 3], [1941, 2], [1946, 1], [1947, 3], [1953, 1], [1958, 3], [1961, 3], [1966, 2], [1976, 3], [1983, 2], [1989, 2], [1993, 1], [1994, 4], [1996, 4], [1998, 2], [2001, 2], [2008, 1], [2010, 3], [2018, 4], [2024, 1], [2030, 4], [2031, 4], [2042, 3], [2044, 1], [2046, 4], [2047, 2], [2056, 4], [2057, 2], [2071, 1], [2075, 1], [2076, 4], [2079, 3], [2080, 1], [2081, 1], [2082, 2], [2083, 3], [2088, 1], [2089, 2], [2090, 2], [2091, 2], [2093, 2], [2107, 3], [2108, 2], [2116, 4], [2119, 4], [2122, 1], [2125, 3], [2128, 4], [2135, 1], [2136, 3], [2140, 3], [2141, 4], [2146, 1], [2147, 2], [2151, 3], [2152, 4], [2154, 4], [2155, 3], [2156, 3], [2160, 3], [2164, 3], [2166, 4], [2167, 1], [2168, 2], [2169, 3], [2171, 2], [2172, 1], [2174, 4], [2176, 2], [2179, 4], [2183, 1], [2189, 3], [2191, 1], [2192, 4], [2197, 3], [2198, 3], [2200, 1], [2204, 2], [2206, 2], [2211, 3], [2216, 2], [2218, 3], [2220, 2], [2222, 4], [2228, 4], [2229, 1], [2231, 1], [2235, 2], [2238, 4], [2241, 2], [2246, 1], [2247, 2], [2250, 1], [2251, 2], [2259, 2], [2262, 2], [2264, 3], [2266, 4], [2268, 4], [2269, 2], [2272, 4], [2273, 4], [2276, 3], [2278, 4], [2279, 1], [2286, 1], [2290, 3], [2292, 3], [2296, 3], [2307, 3], [2310, 4], [2312, 3], [2314, 1], [2318, 1], [2321, 3], [2323, 2], [2325, 4], [2327, 1], [2336, 4], [2344, 2], [2346, 4], [2347, 3], [2349, 2], [2355, 2], [2358, 3], [2361, 2], [2363, 4], [2369, 3], [2372, 2], [2380, 4], [2390, 1], [2392, 4], [2396, 4], [2397, 4], [2400, 3], [2404, 3], [2406, 2], [2408, 3], [2425, 1], [2430, 2], [2436, 2], [2439, 2], [2442, 3], [2451, 1], [2452, 3], [2462, 1], [2464, 1], [2472, 1], [2477, 4], [2478, 1], [2482, 3], [2488, 3], [2491, 1], [2493, 1], [2496, 2], [2499, 1], [2505, 3], [2512, 2], [2514, 3], [2521, 1], [2526, 4], [2530, 1], [2534, 2], [2536, 3], [2537, 4], [2542, 1], [2546, 2], [2548, 4], [2550, 3], [2552, 4], [2556, 3], [2557, 2], [2559, 2], [2560, 2], [2570, 1], [2580, 2], [2584, 2], [2585, 1], [2586, 1], [2589, 1], [2592, 3], [2596, 2]])
Writing time input file: 0.657094
Analysis failed with exit code 201
--------start of stderr-------
--------end of stderr---------
--------start of stdout-------
************************************************************
CalculiX Version 2.11, Copyright(C) 1998-2015 Guido Dhondt
CalculiX comes with ABSOLUTELY NO WARRANTY. This is free
software, and you are welcome to redistribute it under
certain conditions, see gpl.htm
************************************************************
You are using an executable made on So 31. Jul 13:26:31 CEST 2016
The numbers below are estimated upper bounds
number of:
nodes: 2983
elements: 2596
one-dimensional elements: 0
two-dimensional elements: 0
integration points per element: 4
degrees of freedom per node: 3
layers per element: 1
distributed facial loads: 252
distributed volumetric loads: 0
concentrated loads: 0
single point constraints: 312
multiple point constraints: 1
terms in all multiple point constraints: 1
tie constraints: 1
dependent nodes tied by cyclic constraints: 0
dependent nodes in pre-tension constraints: 0
sets: 6
terms in all sets: 9304
materials: 2
constants per material and temperature: 4
temperature points per material: 1
plastic data points per material: 0
orientations: 0
amplitudes: 2
data points in all amplitudes: 2
print requests: 2
transformations: 0
property cards: 0
*INFO: time control parameters set to:
i0 = 4
ir = 8
ip = 9
ic = 200
il = 10
ig = 400
is = 0
ia = 200
ij = 0
it = 0
df = 0.25000000000000000
dc = 0.50000000000000000
db = 0.75000000000000000
da = 0.84999999999999998
ds = 0.0000000000000000
dh = 0.0000000000000000
dd = 1.5000000000000000
wg = 0.0000000000000000
STEP 1
Static analysis was selected
Newton-Raphson iterative procedure is active
Decascading the MPC's
Determining the structure of the matrix:
number of equations
8637
number of nonzero lower triangular matrix elements
269628
increment 1 attempt 1
increment size= 1.000000e-01
sum of previous increments=0.000000e+00
actual step time=1.000000e-01
actual total time=1.000000e-01
iteration 1
Number of contact spring elements=0
Determining the structure of the matrix:
number of equations
8637
number of nonzero lower triangular matrix elements
269628
Using up to 2 cpu(s) for the stress calculation.
Using up to 2 cpu(s) for the symmetric stiffness/mass contributions.
Factoring the system of equations using the symmetric spooles solver
Using up to 2 cpu(s) for spooles.
Using up to 2 cpu(s) for the stress calculation.
average force= 2095.935420
time avg. forc= 2095.935420
largest residual force= 0.000000 in node 2899 and dof 2
largest increment of disp= 5.586546e+00
largest correction to disp= 5.586546e+00 in node 1738 and dof 2
no convergence
iteration 2
Number of contact spring elements=0
Determining the structure of the matrix:
number of equations
8637
number of nonzero lower triangular matrix elements
269628
Using up to 2 cpu(s) for the stress calculation.
Using up to 2 cpu(s) for the symmetric stiffness/mass contributions.
Factoring the system of equations using the symmetric spooles solver
Using up to 2 cpu(s) for spooles.
Using up to 2 cpu(s) for the stress calculation.
average force= 2095.935420
time avg. forc= 2095.935420
largest residual force= 0.000000 in node 2903 and dof 2
largest increment of disp= 5.586546e+00
largest correction to disp= 3.813563e-12 in node 709 and dof 2
convergence
Using up t
--------end of stdout---------
CalculiX failed ccx finished with error 201
```

Word size of OS: 64-bit

Word size of FreeCAD: 64-bit

Version: 0.17.9803 (Git)

Build type: Unknown

Branch: master

Hash: dd63fe92107a87f6003f33518e387743a2090a1c

Python version: 2.7.9

Qt version: 4.8.6

Coin version: 4.0.0a

OCC version: 7.0.0