Hello Everyone,
I am doing a tutorial from abaqus manual on "Analysis of rotating fan using substructure". The manual says that when i run the fansubstr_gen3.inp, it should generate .sup, .sim, .prt, .mdl, .stt, and .odb. But .sup file is not getting generated for me. Could someone please help me with thisAbaqusAbaqus CAEsubstructure 

fansubstr_gen3.inp
*HEADING
Substructure generations: FAN=HUB+4xBLADES  
**
  Z300: a substructure which contains the 1/4 hub 
        and a full blade.
**
**
*NODE
   1,   3.50000,   3.00000,   4.00000   
   3,   3.46638,   3.18024,   4.00000
   7,   3.18024,   3.46638,   4.00000
   9,   3.00000,   3.50000,   4.00000
**  
  28,   6.00000,   3.00000,   4.00000
  30,   5.79830,   4.08144,   4.00000
  34,   4.08144,   5.79830,   4.00000   
  36,   3.00000,   6.00000,   4.00000
**
  82,   6.00000,   3.00000,   0.00000
  84,   5.79830,   4.08144,   0.00000
  88,   4.08144,   5.79830,   0.00000         
  90,   3.00000,   6.00000,   0.00000
**
9998,   3.00000,   3.00000,   4.00000
9999,   3.00000,   3.00000,   0.00000
*NGEN,LINE=C,NSET=NHUB
1,3,1,9998
3,7,1,9998
7,9,1,9998
*NGEN,LINE=C,NSET=RINGF
28,30,1,9998
30,34,1,9998
34,36,1,9998
*NGEN,LINE=C,NSET=RINGB
82,84,1,9999
84,88,1,9999
88,90,1,9999
*NFILL,NSET=HUB
NHUB,RINGF,3,9
RINGF,RINGB,6,9
**
*NODE
  91,   6.34825,   4.61208,   2.00000
  92,   6.04542,   5.17363,   2.04275 
  93,   5.64799,   5.65929,   2.11107
  94,   5.16740,   6.05420,   2.19011
  95,   4.61648,   6.34954,   2.25973
  96,   6.97098,   5.04709,   2.00000
  97,   6.60952,   5.64419,   2.08975
  98,   6.14537,   6.18965,   2.22829
  99,   5.61424,   6.64337,   2.39622
 100,   5.04534,   6.97776,   2.55559
 101,   7.71735,   5.22982,   2.00000
 102,   7.23607,   5.92235,   2.13475
 103,   6.57818,   6.65456,   2.33376
 104,   5.87275,   7.29336,   2.58456
 105,   5.23136,   7.72660,   2.83877
 106,   8.44058,   5.48119,   2.00000
 107,   7.86154,   6.25188,   2.17913
 108,   7.04773,   7.13818,   2.43316
 109,   6.20063,   7.93303,   2.76013
 110,   5.49725,   8.45477,   3.10513
 111,   8.94199,   6.04637,   2.00000
 112,   8.35346,   6.80121,   2.24584
 113,   7.55742,   7.64823,   2.59979
 114,   6.73147,   8.41155,   3.04013
 115,   6.03050,   8.93642,   3.47975
 116,   8.88910,   6.78398,   2.00000
 117,   8.41737,   7.43225,   2.26100
 118,   7.89643,   8.00249,   2.59810
 119,   7.35361,   8.48209,   3.02957
 120,   6.78399,   8.88910,   3.50000
**
*NSET,NSET=NXSYMM,GENERATE
9,90,9
*NSET,NSET=NYSYMM,GENERATE
1,82,9
*NSET,NSET=RETAINED,UNSORTED
  1,   2,   3,   4,   5,   6,   7,   8,   9,  10,
 18,  19,  27,  28,  29,  30,  31,  32,  33,  34,
 35,  36,  37,  45,  46,  54,  55,  63,  64,  72,
 73,  81,  82,  90, 118
**
*ELEMENT,TYPE=S4R
1,1,10,11,2
*ELGEN,ELSET=HUB
1,8,1,1,9,9,8
*ELEMENT,TYPE=S4R
73,57,91,92,58
77,91,96,97,92
*ELGEN,ELSET=CYLBLADE
73,4,1,1
77,4,1,1,5,5,4
**
*ELSET,ELSET=HUBF,GENERATE
1,24,1
*ELSET,ELSET=HUBT,GENERATE
25,72,1
**
*SHELL SECTION,ELSET=HUBF,MATERIAL=MAT
0.250, 3
*SHELL SECTION,ELSET=HUBT,MATERIAL=MAT
0.125, 3
*SHELL SECTION,ELSET=CYLBLADE,MATERIAL=MAT
0.125, 3
*MATERIAL,NAME=MAT
*DENSITY
7850.,
*ELASTIC,TYPE=ISOTROPIC
2.E+11, 0.29
*NSET,NSET=NPRINT,GENERATE
28,36,1
55,63,1
*NSET, NSET=NLOOK
59,93,98,103,108,113,118
**
** PRELOAD 
**
*STEP,NLGEOM
*STATIC
.1,1.
*BOUNDARY
NXSYMM,XSYMM
NYSYMM,YSYMM
NHUB,ENCASTRE
*DLOAD
HUB, CENT, 6.3e6, 3., 3., 0., 0., 0., -1.
CYLBLADE, CENT, 6.3e6, 3., 3., 0., 0., 0., -1.
*EL PRINT,FREQ=0 
*NODE PRINT,NSET=NPRINT,FREQ=100
U,
RF, 
*NODE PRINT, NSET=NLOOK, FREQ=100
U,
RF,
*END STEP
**
*STEP
*FREQUENCY
20,
*BOUNDARY
RETAINED, 1,6
*EL PRINT,FREQ=0 
*NODE PRINT,FREQ=0
*END STEP
**
**
*STEP
*SUBSTRUCTURE GENERATE,TYPE=Z300,LIBRARY=FAN,RECOVERY MATRIX=YES,MASS MATRIX=YES,OVERWRITE
*RETAINED NODAL DOF,SORTED=NO
RETAINED,
** *RETAINED EIGENMODES, GENERATE
** 1,20,1
**
*BOUNDARY,OP=NEW
*SUBSTRUCTURE LOAD CASE,NAME=SPRESS
*DLOAD
CYLBLADE,P,100.
**
*SUBSTRUCTURE LOAD CASE, NAME=SWHOLE
*DLOAD
HUB, CENT, 6.3e6, 3., 3., 0., 0., 0., -1.
CYLBLADE, CENT, 6.3e6, 3., 3., 0., 0., 0., -1.
*END STEP