Console Output

Skipping 617 KB.. Full Log
('An altName of', 'avlAIM_5', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 5
	Name = Wing, index = 1
	Name = hTail, index = 2
	Name = vTail, index = 3
	Name = VTail1, index = 4
	Name = VTail2, index = 5
Getting vortex lattice surface data
	VLM surface name - Wing
	VLM surface name - hTail
	VLM surface name - vTail
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 4 (ID = 3)
	Section 2 of 4 (ID = 2)
	Section 3 of 4 (ID = 1)
	Section 4 of 4 (ID = 0)
Writing surface - hTail (ID = 1)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - vTail (ID = 2)
	Section 1 of 2 (ID = 0)
	Section 2 of 2 (ID = 1)


Running avl......
. Cleaning up avlInstance - 0
 Cleaning up avlInstance - 1
 Cleaning up avlInstance - 2
 Cleaning up avlInstance - 3
 Cleaning up avlInstance - 4
 Cleaning up avlInstance - 5
 EGADS Info: 82 Objects, 103 Reference in Use (of 3382) at Close!
 EGADS Info: 5 unattached Objects (103 References) removed!
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
Analysis directory does not currently exist - it will be made automatically
 CAPS Info: No symbol for aimDiscr in egadsTessAIM
 CAPS Info: No symbol for aimFreeDiscr in egadsTessAIM
 CAPS Info: No symbol for aimLocateElement in egadsTessAIM
 CAPS Info: No symbol for aimUsesDataSet in egadsTessAIM
 CAPS Info: No symbol for aimCheck in egadsTessAIM
 CAPS Info: No symbol for aimTransfer in egadsTessAIM
 CAPS Info: No symbol for aimInterpolation in egadsTessAIM
 CAPS Info: No symbol for aimInterpolateBar in egadsTessAIM
 CAPS Info: No symbol for aimIntegration in egadsTessAIM
 CAPS Info: No symbol for aimIntegrateBar in egadsTessAIM
 CAPS Info: No symbol for aimSensitivity in egadsTessAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] set:            cmean  sqrt(area/aspect)
                          cmean =     2.82843     0.00000
    executing [   2] set:            span  cmean*aspect
                          span =    14.14214     0.00000
    executing [   3] set:            sspan  span/2
                          sspan =     7.07107     0.00000
    executing [   4] set:            croot  2*cmean/(1+taper)
                          croot =     3.77124     0.00000
    executing [   5] set:            ctip  croot*taper
                          ctip =     1.88562     0.00000
    executing [   6] set:            xtip  sspan*tand(lesweep)
                          xtip =     4.08248     0.00000
    executing [   7] set:            ytip  sspan*tand(dihedral)
                          ytip =     0.12343     0.00000
    executing [   8] set:            ybot  -0.1*croot
                          ybot =    -0.37712     0.00000
    executing [   9] set:            ytop  +0.2*croot+ytip
                          ytop =     0.87767     0.00000
    executing [  10] set:            extend  0.02*cmean
                          extend =     0.05657     0.00000
    executing [  11] mark:
                          Mark        created
    executing [  12] udprim:     naca Series  8412.00000 (compiled code)
                          Body      1 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  13] scale:          3.77124      0.00000      0.00000      0.00000
                          Body      2 created  (toler= 3.7712e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  14] udprim:     naca Series    20.00000 (compiled code)
                          Body      3 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  15] scale:          1.88562      0.00000      0.00000      0.00000
                          Body      4 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  16] rotatez:      -15.00000      0.00000      0.00000
                          Body      5 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  17] translate:      4.08248      0.12343     -7.07107
                          Body      6 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  18] rule:           0.00000      0.00000
                          ruling  2 Xsects with 3 Strips each...
                          Body      7 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  19] store:      HalfWing      0.00000      0.00000
                          Body      7 stored
    executing [  20] restore:    HalfWing      0.00000
                          Body      8 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  21] restore:    HalfWing      0.00000
                          Body      9 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  22] mirror:         0.00000      0.00000      1.00000      0.00000
                          Body     10 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  23] join:           0.00000      0.00000
                          Body     11 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  24] rotatex:       90.00000      0.00000      0.00000
                          Body     12 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  25] store:      Wing      0.00000      0.00000
                          Body     12 stored
    executing [  26] restore:    Wing      0.00000
                          Body     13 restored (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  27] restore:    Wing      0.00000
                          Body     14 restored (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  28] scale:          0.40000      0.00000      0.00000      0.00000
                          Body     15 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  29] translate:     10.00000      0.00000      0.00000
                          Body     16 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  30] sphere:         0.00000      0.00000      0.00000     80.00000
                          Body     17 created  (toler= 1.0000e-05, nnode=   2, nedge=   6, nface=   2)
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    sphere                    1       0.007    1.0
    udprim                    2       0.027    3.8
    restore                   4       0.023    3.2
    rule                      1       0.142   20.1
    join                      1       0.134   18.9
    translate                 2       0.105   14.8
    rotatex                   1       0.106   15.0
    rotatez                   1       0.004    0.6
    scale                     3       0.116   16.4
    mirror                    1       0.029    4.1
    set                      10       0.011    1.6
    store                     2       0.003    0.4
    mark                      1       0.001    0.1
    Total                    30       0.708
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 3)
	Tessellating body
Number of nodes = 9665
Number of elements = 19326
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19326
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 3)
	Tessellating body
Number of nodes = 6110
Number of elements = 12216
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 12216
Number of quadrilateral elements = 0
Getting surface mesh for body 3 (of 3)
	Tessellating body
Number of nodes = 108
Number of elements = 212
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 212
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 15883
Total number of elements = 31754
.Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
 CAPS Info: No symbol for aimDiscr in egadsTessAIM
 CAPS Info: No symbol for aimFreeDiscr in egadsTessAIM
 CAPS Info: No symbol for aimLocateElement in egadsTessAIM
 CAPS Info: No symbol for aimUsesDataSet in egadsTessAIM
 CAPS Info: No symbol for aimCheck in egadsTessAIM
 CAPS Info: No symbol for aimTransfer in egadsTessAIM
 CAPS Info: No symbol for aimInterpolation in egadsTessAIM
 CAPS Info: No symbol for aimInterpolateBar in egadsTessAIM
 CAPS Info: No symbol for aimIntegration in egadsTessAIM
 CAPS Info: No symbol for aimIntegrateBar in egadsTessAIM
 CAPS Info: No symbol for aimSensitivity in egadsTessAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] set:            cmean  sqrt(area/aspect)
                          cmean =     2.82843     0.00000
    executing [   2] set:            span  cmean*aspect
                          span =    14.14214     0.00000
    executing [   3] set:            sspan  span/2
                          sspan =     7.07107     0.00000
    executing [   4] set:            croot  2*cmean/(1+taper)
                          croot =     3.77124     0.00000
    executing [   5] set:            ctip  croot*taper
                          ctip =     1.88562     0.00000
    executing [   6] set:            xtip  sspan*tand(lesweep)
                          xtip =     4.08248     0.00000
    executing [   7] set:            ytip  sspan*tand(dihedral)
                          ytip =     0.12343     0.00000
    executing [   8] set:            ybot  -0.1*croot
                          ybot =    -0.37712     0.00000
    executing [   9] set:            ytop  +0.2*croot+ytip
                          ytop =     0.87767     0.00000
    executing [  10] set:            extend  0.02*cmean
                          extend =     0.05657     0.00000
    executing [  11] mark:
                          Mark        created
    executing [  12] udprim:     naca Series  8412.00000 (compiled code)
                          Body      1 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  13] scale:          3.77124      0.00000      0.00000      0.00000
                          Body      2 created  (toler= 3.7712e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  14] udprim:     naca Series    20.00000 (compiled code)
                          Body      3 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  15] scale:          1.88562      0.00000      0.00000      0.00000
                          Body      4 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  16] rotatez:      -15.00000      0.00000      0.00000
                          Body      5 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  17] translate:      4.08248      0.12343     -7.07107
                          Body      6 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  18] rule:           0.00000      0.00000
                          ruling  2 Xsects with 3 Strips each...
                          Body      7 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  19] store:      HalfWing      0.00000      0.00000
                          Body      7 stored
    executing [  20] restore:    HalfWing      0.00000
                          Body      8 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  21] restore:    HalfWing      0.00000
                          Body      9 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  22] mirror:         0.00000      0.00000      1.00000      0.00000
                          Body     10 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  23] join:           0.00000      0.00000
                          Body     11 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  24] rotatex:       90.00000      0.00000      0.00000
                          Body     12 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  25] store:      Wing      0.00000      0.00000
                          Body     12 stored
    executing [  26] box:          -40.00000    -40.00000    -40.00000     80.00000     80.00000     80.00000
                          Body     13 created  (toler= 1.0000e-07, nnode=   8, nedge=  12, nface=   6)
    executing [  27] restore:    Wing      0.00000
                          Body     14 restored (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  28] subtract:   none      1.00000   0.0000e+00
                          Body     15 created  (toler= 1.0000e-07, nnode=  17, nedge=  27, nface=  14)
    executing [  29] select:   body
                    putting Branch Attributes on Body
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    box                       1       0.003    0.4
    udprim                    2       0.025    3.2
    restore                   3       0.009    1.2
    rule                      1       0.118   15.2
    subtract                  1       0.158   20.4
    join                      1       0.297   38.4
    translate                 1       0.003    0.4
    rotatex                   1       0.103   13.3
    rotatez                   1       0.004    0.5
    scale                     2       0.006    0.8
    mirror                    1       0.031    4.0
    set                      10       0.015    1.9
    select                    1       0.000    0.0
    store                     2       0.001    0.1
    mark                      1       0.001    0.1
    Total                    29       0.774
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
	Tessellating body
Number of nodes = 9693
Number of elements = 19378
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19378
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9693
Total number of elements = 19378
.Analysis directory does not currently exist - it will be made automatically
 CAPS Info: No symbol for aimDiscr in egadsTessAIM
 CAPS Info: No symbol for aimFreeDiscr in egadsTessAIM
 CAPS Info: No symbol for aimLocateElement in egadsTessAIM
 CAPS Info: No symbol for aimUsesDataSet in egadsTessAIM
 CAPS Info: No symbol for aimCheck in egadsTessAIM
 CAPS Info: No symbol for aimTransfer in egadsTessAIM
 CAPS Info: No symbol for aimInterpolation in egadsTessAIM
 CAPS Info: No symbol for aimInterpolateBar in egadsTessAIM
 CAPS Info: No symbol for aimIntegration in egadsTessAIM
 CAPS Info: No symbol for aimIntegrateBar in egadsTessAIM
 CAPS Info: No symbol for aimSensitivity in egadsTessAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] set:            meshingAIMs  $pointwiseAIM;aflr4AIM;egadsTessAIM
                          meshingAIMs = $pointwiseAIM;aflr4AIM;egadsTessAIM
    executing [   2] box:            0.00000     -0.50000     -0.50000      1.00000      1.00000      1.00000
                          Body      1 created  (toler= 1.0000e-07, nnode=   8, nedge=  12, nface=   6)
    executing [   3] select:   edge  1
                     putting Branch Attributes on Edge 1
    executing [   4] box:            2.00000      0.00000      0.00000      1.00000      0.00000      0.50000
                          Body      2 created  (toler= 1.0000e-07, nnode=   4, nedge=   4, nface=   1)
    executing [   5] revolve:        2.00000      0.00000      0.00000      1.00000      0.00000      0.00000    360.00000
WARNING:: jbody= 2, jnode= 1, ibody= 3, found= 1, dbest= 0.500000000 (revolve)
WARNING:: jbody= 2, jnode= 2, ibody= 3, found= 2, dbest= 0.500000000 (revolve)
                          Body      3 created  (toler= 1.0000e-07, nnode=   2, nedge=   3, nface=   3)
    executing [   6] cone:           4.00000      0.00000      0.00000      5.00000      0.00000      0.00000      0.50000
                          Body      4 created  (toler= 1.0000e-05, nnode=   3, nedge=   6, nface=   3)
    executing [   7] skbeg:          7.00000      0.00000      0.00000      0.00000
    executing [   8] linseg:         7.25000      0.00000      0.00000
    executing [   9] skend:          0.00000
                          Sketch    7 created with 1 Edges
    executing [  10] revolve:        7.00000      0.00000      0.00000      0.00000      1.00000      0.00000    360.00000
WARNING:: jbody= 7, jnode= 1, ibody= 8, found= 1, dbest= 0.250000000 (revolve)
                          Body      8 created  (toler= 1.0000e-07, nnode=   1, nedge=   1, nface=   1)
    executing [  11] revolve:        6.50000      0.00000      0.00000      0.00000      0.00000      1.00000    360.00000
                          Body      9 created  (toler= 1.0000e-07, nnode=   1, nedge=   2, nface=   1)
    executing [  12] select:   edge  1
                     putting Branch Attributes on Edge 1
    executing [  13] select:   edge  2
                     putting Branch Attributes on Edge 2
    executing [  14] sphere:         8.50000      0.00000      0.00000      0.50000
                          Body     10 created  (toler= 1.0000e-05, nnode=   2, nedge=   6, nface=   2)
    executing [  15] box:           10.00000     -0.50000     -0.50000      1.00000      1.00000      1.00000
                          Body     11 created  (toler= 1.0000e-07, nnode=   8, nedge=  12, nface=   6)
    executing [  16] cylinder:      10.50000      0.00000     -1.00000     10.50000      0.00000      1.00000      0.25000
                          Body     12 created  (toler= 1.0000e-05, nnode=   4, nedge=   6, nface=   4)
    executing [  17] subtract:   none      1.00000   0.0000e+00
                          Body     13 created  (toler= 1.0000e-05, nnode=  12, nedge=  18, nface=   8)
    executing [  18] box:           10.50000      0.00000     -1.00000      1.00000      0.00000      2.00000
                          Body     14 created  (toler= 1.0000e-07, nnode=   4, nedge=   4, nface=   1)
    executing [  19] subtract:   none      1.00000   0.0000e+00
                          Body     15 created  (toler= 1.0000e-05, nnode=  14, nedge=  23, nface=   9)
    executing [  20] select:   body
                    putting Branch Attributes on Body
    executing [  21] select:   face
                     putting Branch Attributes on Face 1
                     putting Branch Attributes on Face 2
                     putting Branch Attributes on Face 3
                     putting Branch Attributes on Face 4
                     putting Branch Attributes on Face 5
                     putting Branch Attributes on Face 6
                     putting Branch Attributes on Face 7
                     putting Branch Attributes on Face 8
                     putting Branch Attributes on Face 9
    executing [  22] set:            fs:radius  0.5
                          fs:radius =     0.50000     0.00000
    executing [  23] set:            fs:nose:radius  0.25
                          fs:nose:radius =     0.25000     0.00000
    executing [  24] set:            fs:nose:ogive_radius  10.0
                          fs:nose:ogive_radius =    10.00000     0.00000
    executing [  25] skbeg:         12.00000      0.00000      0.00000      1.00000
    executing [  26] skvar:   xy      0.00000      0.00000      0.00000 ...
    -> creating  ::x[1] =    0.00000
    -> creating  ::y[1] =    0.00000
    -> creating  ::x[2] =    0.07000
    -> creating  ::y[2] =   -0.12000
    -> creating  ::d[2] =    0.02000
    -> creating  ::x[3] =    1.00000
    -> creating  ::y[3] =   -0.50000
    -> creating  ::d[3] =    0.09000
    -> creating  ::x[4] =    1.00000
    -> creating  ::y[4] =    0.00000
    executing [  27] skcon:   X    1   -1  0
    executing [  28] skcon:   Y    1   -1  0
    executing [  29] skcon:   P    1   -1  0
    executing [  30] skcon:   R    1    2  fs:nose:radius
    executing [  31] skcon:   T    2   -1  0
    executing [  32] skcon:   R    2    3  fs:nose:ogive_radius
    executing [  33] skcon:   V    3    4  0
    executing [  34] skcon:   P    4   -1  0
    executing [  35] skcon:   L    3    4  fs:radius
    executing [  36] skcon:   H    4    1  0
    -> solving   iter =   0,   f0max =   8.5532e+00   accepting, omega=   0.30000
ERROR:: BAD STATUS = -276 from matsol (called from solveSketchOrig:46965)
trying Levenberg-Marquardt solver
    -> solving   iter =   0,   f0max =   8.5532e+00
    -> solving   iter =   1,   f0max =   1.6117e+01
    -> solving   iter =   2,   f0max =   1.7448e+01
    -> solving   iter =   3,   f0max =   1.9375e+01
    -> solving   iter =   4,   f0max =   2.2607e+01
    -> solving   iter =   5,   f0max =   3.0533e+01
    -> solving   iter =   6,   f0max =   1.0148e+02
    -> solving   iter =   7,   f0max =   1.6544e+01
    -> solving   iter =   8,   f0max =   2.5075e-01
    -> solving   iter =   9,   f0max =   2.3231e-01
    -> solving   iter =  10,   f0max =   2.0847e-01
    -> solving   iter =  11,   f0max =   1.8155e-01
    -> solving   iter =  12,   f0max =   1.5222e-01
    -> solving   iter =  13,   f0max =   1.2009e-01
    -> solving   iter =  14,   f0max =   9.7602e-02
    -> solving   iter =  15,   f0max =   6.4364e-02
    -> solving   iter =  16,   f0max =   4.0512e-02
    -> solving   iter =  17,   f0max =   2.1157e-02
    -> solving   iter =  18,   f0max =   7.5481e-03
    -> solving   iter =  19,   f0max =   1.7629e-03
    -> solving   iter =  20,   f0max =   2.3639e-04
    -> solving   iter =  21,   f0max =   1.6881e-05
    -> solving   iter =  22,   f0max =   6.2000e-07
    -> solving   iter =  23,   f0max =   1.1572e-08
    -> solving   iter =  24,   f0max =   1.0905e-10
    -> updating  ::x[1] =   -0.00000
    -> updating  ::y[1] =    0.00000
    -> updating  ::x[2] =    0.18062
    -> updating  ::y[2] =   -0.24018
    -> updating  ::d[2] =    0.05019
    -> updating  ::x[3] =    1.33041
    -> updating  ::y[3] =   -0.50000
    -> updating  ::d[3] =    0.01738
    -> updating  ::x[4] =    1.33041
    -> updating  ::y[4] =   -0.00000
    executing [  37] arc:            0.18062     -0.24018      0.00000      0.05019  xy
    executing [  38] arc:            1.33041     -0.50000      0.00000      0.01738  xy
    executing [  39] linseg:         1.33041     -0.00000      0.00000
    executing [  40] linseg:        -0.00000      0.00000      0.00000
    executing [  41] skend:          0.00000
                          Sketch   21 created with 4 Edges
    executing [  42] revolve:        0.00000      0.00000      0.00000      1.00000      0.00000      0.00000    360.00000
WARNING:: jbody=21, jnode= 4, ibody=22, found= 3, dbest= 0.500000000 (revolve)
                          Body     22 created  (toler= 1.0000e-07, nnode=   3, nedge=   5, nface=   3)
    executing [  43] select:   body
                    putting Branch Attributes on Body
    executing [  44] select:   face
                     putting Branch Attributes on Face 1
                     putting Branch Attributes on Face 2
                     putting Branch Attributes on Face 3
    executing [  45] box:           -1.00000     -2.00000     -2.00000     15.00000      4.00000      4.00000
                          Body     23 created  (toler= 1.0000e-07, nnode=   8, nedge=  12, nface=   6)
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    box                       5       0.022    5.5
    sphere                    1       0.008    2.0
    cone                      1       0.005    1.3
    cylinder                  1       0.011    2.8
    revolve                   4       0.175   43.8
    subtract                  2       0.088   22.0
    skbeg                     2       0.002    0.5
    skvar                     1       0.003    0.8
    skcon                    10       0.003    0.8
    linseg                    3       0.003    0.8
    arc                       2       0.000    0.0
    skend                     2       0.006    1.5
    set                       4       0.006    1.5
    select                    7       0.068   17.0
    Total                    45       0.400
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 8
	Name = box, index = 1
	Name = cylinder, index = 2
	Name = cone, index = 3
	Name = torus, index = 4
	Name = sphere, index = 5
	Name = boxhole, index = 6
	Name = bullet, index = 7
	Name = farfield, index = 8
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 8)
	Tessellating body
Number of nodes = 1538
Number of elements = 3072
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 8)
	Tessellating body
Number of nodes = 876
Number of elements = 1748
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1748
Number of quadrilateral elements = 0
Getting surface mesh for body 3 (of 8)
	Tessellating body
Number of nodes = 1319
Number of elements = 2634
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2634
Number of quadrilateral elements = 0
Getting surface mesh for body 4 (of 8)
	Tessellating body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of nodes = 2048
Number of elements = 4096
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Getting surface mesh for body 5 (of 8)
	Tessellating body
Number of nodes = 847
Number of elements = 1690
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1690
Number of quadrilateral elements = 0
Getting surface mesh for body 6 (of 8)
	Tessellating body
 570 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 570 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 570 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 570 EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Number of nodes = 1961
Number of elements = 3922
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3922
Number of quadrilateral elements = 0
Getting surface mesh for body 7 (of 8)
	Tessellating body
Number of nodes = 933
Number of elements = 1862
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1862
Number of quadrilateral elements = 0
Getting surface mesh for body 8 (of 8)
	Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 83252
Total number of elements = 166480
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_1', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
	Tessellating body
Number of nodes = 1538
Number of elements = 3072
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3072
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
	Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75268
Total number of elements = 150528
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_2', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = boxhole, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
	Tessellating body
 570 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 4 7, sen = -1!
 570 EGADS Info: Face #3 -> Edge #9 (9) Internally in Loop 7 4, sen = 1!
 FAC EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 7 4, sen = -1!
 FAC EGADS Info: Face #5 -> Edge #17 (9) Internally in Loop 4 7, sen = 1!
Number of nodes = 1961
Number of elements = 3922
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 3922
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
	Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75691
Total number of elements = 151378
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_3', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = bullet, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
	Tessellating body
Number of nodes = 933
Number of elements = 1862
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1862
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
	Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74663
Total number of elements = 149318
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_4', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cone, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
	Tessellating body
Number of nodes = 1319
Number of elements = 2634
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 2634
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
	Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75049
Total number of elements = 150090
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_5', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = cylinder, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
	Tessellating body
Number of nodes = 876
Number of elements = 1748
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1748
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
	Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74606
Total number of elements = 149204
.Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
 CAPS Info: No symbol for aimDiscr in egadsTessAIM
 CAPS Info: No symbol for aimFreeDiscr in egadsTessAIM
 CAPS Info: No symbol for aimLocateElement in egadsTessAIM
 CAPS Info: No symbol for aimUsesDataSet in egadsTessAIM
 CAPS Info: No symbol for aimCheck in egadsTessAIM
 CAPS Info: No symbol for aimTransfer in egadsTessAIM
 CAPS Info: No symbol for aimInterpolation in egadsTessAIM
 CAPS Info: No symbol for aimInterpolateBar in egadsTessAIM
 CAPS Info: No symbol for aimIntegration in egadsTessAIM
 CAPS Info: No symbol for aimIntegrateBar in egadsTessAIM
 CAPS Info: No symbol for aimSensitivity in egadsTessAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] set:            cmean  sqrt(area/aspect)
                          cmean =     2.82843     0.00000
    executing [   2] set:            span  cmean*aspect
                          span =    14.14214     0.00000
    executing [   3] set:            sspan  span/2
                          sspan =     7.07107     0.00000
    executing [   4] set:            croot  2*cmean/(1+taper)
                          croot =     3.77124     0.00000
    executing [   5] set:            ctip  croot*taper
                          ctip =     1.88562     0.00000
    executing [   6] set:            xtip  sspan*tand(lesweep)
                          xtip =     4.08248     0.00000
    executing [   7] set:            ytip  sspan*tand(dihedral)
                          ytip =     0.12343     0.00000
    executing [   8] set:            ybot  -0.1*croot
                          ybot =    -0.37712     0.00000
    executing [   9] set:            ytop  +0.2*croot+ytip
                          ytop =     0.87767     0.00000
    executing [  10] set:            extend  0.02*cmean
                          extend =     0.05657     0.00000
    executing [  11] mark:
                          Mark        created
    executing [  12] udprim:     naca Series  8412.00000 (compiled code)
                          Body      1 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  13] scale:          3.77124      0.00000      0.00000      0.00000
                          Body      2 created  (toler= 3.7712e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  14] udprim:     naca Series    20.00000 (compiled code)
                          Body      3 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  15] scale:          1.88562      0.00000      0.00000      0.00000
                          Body      4 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  16] rotatez:      -15.00000      0.00000      0.00000
                          Body      5 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  17] translate:      4.08248      0.12343     -7.07107
                          Body      6 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  18] rule:           0.00000      0.00000
                          ruling  2 Xsects with 3 Strips each...
                          Body      7 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  19] store:      HalfWing      0.00000      0.00000
                          Body      7 stored
    executing [  20] restore:    HalfWing      0.00000
                          Body      8 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  21] restore:    HalfWing      0.00000
                          Body      9 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  22] mirror:         0.00000      0.00000      1.00000      0.00000
                          Body     10 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  23] join:           0.00000      0.00000
                          Body     11 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  24] rotatex:       90.00000      0.00000      0.00000
                          Body     12 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  25] store:      Wing      0.00000      0.00000
                          Body     12 stored
    executing [  26] box:          -40.00000    -40.00000    -40.00000     80.00000     80.00000     80.00000
                          Body     13 created  (toler= 1.0000e-07, nnode=   8, nedge=  12, nface=   6)
    executing [  27] restore:    Wing      0.00000
                          Body     14 restored (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  28] subtract:   none      1.00000   0.0000e+00
                          Body     15 created  (toler= 1.0000e-07, nnode=  17, nedge=  27, nface=  14)
    executing [  29] select:   body
                    putting Branch Attributes on Body
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    box                       1       0.013    2.1
    udprim                    2       0.019    3.1
    restore                   3       0.012    1.9
    rule                      1       0.108   17.4
    subtract                  1       0.167   27.0
    join                      1       0.147   23.7
    translate                 1       0.003    0.5
    rotatex                   1       0.104   16.8
    rotatez                   1       0.002    0.3
    scale                     2       0.006    1.0
    mirror                    1       0.029    4.7
    set                      10       0.003    0.5
    select                    1       0.001    0.2
    store                     2       0.005    0.8
    mark                      1       0.000    0.0
    Total                    29       0.619
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
**********************************************************
Mesh_Length_Factor is: -1.000000
Mesh_Length_Factor must be a positive number.
**********************************************************
Error: egadsTessAIM (instance = 0) status -311
.Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
 CAPS Info: No symbol for aimDiscr in egadsTessAIM
 CAPS Info: No symbol for aimFreeDiscr in egadsTessAIM
 CAPS Info: No symbol for aimLocateElement in egadsTessAIM
 CAPS Info: No symbol for aimUsesDataSet in egadsTessAIM
 CAPS Info: No symbol for aimCheck in egadsTessAIM
 CAPS Info: No symbol for aimTransfer in egadsTessAIM
 CAPS Info: No symbol for aimInterpolation in egadsTessAIM
 CAPS Info: No symbol for aimInterpolateBar in egadsTessAIM
 CAPS Info: No symbol for aimIntegration in egadsTessAIM
 CAPS Info: No symbol for aimIntegrateBar in egadsTessAIM
 CAPS Info: No symbol for aimSensitivity in egadsTessAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] set:            cmean  sqrt(area/aspect)
                          cmean =     2.82843     0.00000
    executing [   2] set:            span  cmean*aspect
                          span =    14.14214     0.00000
    executing [   3] set:            sspan  span/2
                          sspan =     7.07107     0.00000
    executing [   4] set:            croot  2*cmean/(1+taper)
                          croot =     3.77124     0.00000
    executing [   5] set:            ctip  croot*taper
                          ctip =     1.88562     0.00000
    executing [   6] set:            xtip  sspan*tand(lesweep)
                          xtip =     4.08248     0.00000
    executing [   7] set:            ytip  sspan*tand(dihedral)
                          ytip =     0.12343     0.00000
    executing [   8] set:            ybot  -0.1*croot
                          ybot =    -0.37712     0.00000
    executing [   9] set:            ytop  +0.2*croot+ytip
                          ytop =     0.87767     0.00000
    executing [  10] set:            extend  0.02*cmean
                          extend =     0.05657     0.00000
    executing [  11] mark:
                          Mark        created
    executing [  12] udprim:     naca Series  8412.00000 (compiled code)
                          Body      1 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  13] scale:          3.77124      0.00000      0.00000      0.00000
                          Body      2 created  (toler= 3.7712e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  14] udprim:     naca Series    20.00000 (compiled code)
                          Body      3 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  15] scale:          1.88562      0.00000      0.00000      0.00000
                          Body      4 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  16] rotatez:      -15.00000      0.00000      0.00000
                          Body      5 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  17] translate:      4.08248      0.12343     -7.07107
                          Body      6 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  18] rule:           0.00000      0.00000
                          ruling  2 Xsects with 3 Strips each...
                          Body      7 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  19] store:      HalfWing      0.00000      0.00000
                          Body      7 stored
    executing [  20] restore:    HalfWing      0.00000
                          Body      8 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  21] restore:    HalfWing      0.00000
                          Body      9 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  22] mirror:         0.00000      0.00000      1.00000      0.00000
                          Body     10 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  23] join:           0.00000      0.00000
                          Body     11 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  24] rotatex:       90.00000      0.00000      0.00000
                          Body     12 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  25] store:      Wing      0.00000      0.00000
                          Body     12 stored
    executing [  26] box:          -40.00000    -40.00000    -40.00000     80.00000     80.00000     80.00000
                          Body     13 created  (toler= 1.0000e-07, nnode=   8, nedge=  12, nface=   6)
    executing [  27] restore:    Wing      0.00000
                          Body     14 restored (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  28] subtract:   none      1.00000   0.0000e+00
                          Body     15 created  (toler= 1.0000e-07, nnode=  17, nedge=  27, nface=  14)
    executing [  29] select:   body
                    putting Branch Attributes on Body
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    box                       1       0.005    0.8
    udprim                    2       0.020    3.1
    restore                   3       0.016    2.5
    rule                      1       0.127   19.8
    subtract                  1       0.171   26.7
    join                      1       0.138   21.6
    translate                 1       0.003    0.5
    rotatex                   1       0.106   16.6
    rotatez                   1       0.002    0.3
    scale                     2       0.005    0.8
    mirror                    1       0.035    5.5
    set                      10       0.006    0.9
    select                    1       0.001    0.2
    store                     2       0.005    0.8
    mark                      1       0.000    0.0
    Total                    29       0.640
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
	Tessellating body
Number of nodes = 9693
Number of elements = 19378
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 19378
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 9693
Total number of elements = 19378
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 2
	Name = Farfield, index = 1
	Name = Wing1, index = 2

Getting mesh sizing parameters
	Mesh sizing name - Farfield
	Done getting mesh sizing parameters
Getting surface mesh for body 1 (of 1)
	Tessellating body
Number of nodes = 7188
Number of elements = 14368
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 14368
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 7188
Total number of elements = 14368
.Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
 CAPS Info: No symbol for aimDiscr in egadsTessAIM
 CAPS Info: No symbol for aimFreeDiscr in egadsTessAIM
 CAPS Info: No symbol for aimLocateElement in egadsTessAIM
 CAPS Info: No symbol for aimUsesDataSet in egadsTessAIM
 CAPS Info: No symbol for aimCheck in egadsTessAIM
 CAPS Info: No symbol for aimTransfer in egadsTessAIM
 CAPS Info: No symbol for aimInterpolation in egadsTessAIM
 CAPS Info: No symbol for aimInterpolateBar in egadsTessAIM
 CAPS Info: No symbol for aimIntegration in egadsTessAIM
 CAPS Info: No symbol for aimIntegrateBar in egadsTessAIM
 CAPS Info: No symbol for aimSensitivity in egadsTessAIM
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_6', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = sphere, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
	Tessellating body
Number of nodes = 847
Number of elements = 1690
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 1690
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
	Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 74577
Total number of elements = 149146
.
Analysis object with the name, egadsTessAIM, has already been initilized
('An altName of', 'egadsTessAIM_7', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = torus, index = 1
	Name = farfield, index = 2
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 0
Getting surface mesh for body 1 (of 2)
	Tessellating body
Warning: No capsGroup/capsIgnore attribute found on edge 1 of face 1, unable to assign a boundary index value
Warning: No capsGroup/capsIgnore attribute found on edge 2 of face 1, unable to assign a boundary index value
Number of nodes = 2048
Number of elements = 4096
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 4096
Number of quadrilateral elements = 0
Getting surface mesh for body 2 (of 2)
	Tessellating body
Number of nodes = 73730
Number of elements = 147456
Number of node elements = 0
Number of line elements = 0
Number of triangle elements = 147456
Number of quadrilateral elements = 0
----------------------------
Total number of nodes = 75778
Total number of elements = 151552
. Cleaning up egadsInstance - 0
 Cleaning up egadsInstance - 1
 Cleaning up egadsInstance - 2
 Cleaning up egadsInstance - 3
 Cleaning up egadsInstance - 4
 Cleaning up egadsInstance - 5
 Cleaning up egadsInstance - 6
 Cleaning up egadsInstance - 7
 EGADS Info: 0 Objects, 0 Reference in Use (of 1494) at Close!
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
Analysis directory does not currently exist - it will be made automatically
 CAPS Info: No symbol for aimExecute in fun3dAIM
 CAPS Info: No symbol for aimCheck in fun3dAIM
 CAPS Info: No symbol for aimData in fun3dAIM
 CAPS Info: No symbol for aimSensitivity in fun3dAIM

Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_1', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] set:            cmean  sqrt(area/aspect)
                          cmean =     2.82843     0.00000
    executing [   2] set:            span  cmean*aspect
                          span =    14.14214     0.00000
    executing [   3] set:            sspan  span/2
                          sspan =     7.07107     0.00000
    executing [   4] set:            croot  2*cmean/(1+taper)
                          croot =     3.77124     0.00000
    executing [   5] set:            ctip  croot*taper
                          ctip =     1.88562     0.00000
    executing [   6] set:            xtip  sspan*tand(lesweep)
                          xtip =     4.08248     0.00000
    executing [   7] set:            ytip  sspan*tand(dihedral)
                          ytip =     0.12343     0.00000
    executing [   8] set:            ybot  -0.1*croot
                          ybot =    -0.37712     0.00000
    executing [   9] set:            ytop  +0.2*croot+ytip
                          ytop =     0.87767     0.00000
    executing [  10] set:            extend  0.02*cmean
                          extend =     0.05657     0.00000
    executing [  11] mark:
                          Mark        created
    executing [  12] udprim:     naca Series  8412.00000 (compiled code)
                          Body      1 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  13] scale:          3.77124      0.00000      0.00000      0.00000
                          Body      2 created  (toler= 3.7712e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  14] udprim:     naca Series    20.00000 (compiled code)
                          Body      3 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  15] scale:          1.88562      0.00000      0.00000      0.00000
                          Body      4 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  16] rotatez:      -15.00000      0.00000      0.00000
                          Body      5 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  17] translate:      4.08248      0.12343     -7.07107
                          Body      6 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  18] rule:           0.00000      0.00000
                          ruling  2 Xsects with 3 Strips each...
                          Body      7 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  19] store:      HalfWing      0.00000      0.00000
                          Body      7 stored
    executing [  20] restore:    HalfWing      0.00000
                          Body      8 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  21] restore:    HalfWing      0.00000
                          Body      9 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  22] mirror:         0.00000      0.00000      1.00000      0.00000
                          Body     10 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  23] join:           0.00000      0.00000
                          Body     11 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  24] rotatex:       90.00000      0.00000      0.00000
                          Body     12 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  25] store:      Wing      0.00000      0.00000
                          Body     12 stored
    executing [  26] restore:    Wing      0.00000
                          Body     13 restored (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  27] restore:    Wing      0.00000
                          Body     14 restored (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  28] scale:          0.40000      0.00000      0.00000      0.00000
                          Body     15 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  29] translate:     10.00000      0.00000      0.00000
                          Body     16 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  30] sphere:         0.00000      0.00000      0.00000     80.00000
                          Body     17 created  (toler= 1.0000e-05, nnode=   2, nedge=   6, nface=   2)
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    sphere                    1       0.006    0.8
    udprim                    2       0.024    3.4
    restore                   4       0.021    2.9
    rule                      1       0.120   16.8
    join                      1       0.147   20.6
    translate                 2       0.113   15.8
    rotatex                   1       0.113   15.8
    rotatez                   1       0.003    0.4
    scale                     3       0.111   15.6
    mirror                    1       0.043    6.0
    set                      10       0.007    1.0
    store                     2       0.004    0.6
    mark                      1       0.001    0.1
    Total                    30       0.713
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Warning: No boundary condition specified for capsGroup Wing2!
	Warning: No boundary condition specified for capsGroup Farfield!
	Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.

Using Python to write FUN3D namelist (fun3d.nml)

	Reading fun3d.nml .....
	Appending namelist
	Done writing nml file with Python

.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_2', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Warning: No boundary condition specified for capsGroup Wing2!
	Warning: No boundary condition specified for capsGroup Farfield!
	Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.

Using Python to write FUN3D namelist (fun3d.nml)

	Reading fun3d.nml .....
	Error: Python error occurred while writing namelist file
Traceback (most recent call last):
  File "fun3dNamelist.pyx", line 88, in fun3dNamelist.fun3d_writeNMLPython
  File "fun3dNamelist.pyx", line 61, in fun3dNamelist.read_fun3d_nml
  File "C:\Users\jenkins\ESP_Python37\lib\site-packages\f90nml\__init__.py", line 31, in read
    return parser.read(nml_path)
  File "C:\Users\jenkins\ESP_Python37\lib\site-packages\f90nml\parser.py", line 264, in read
    return self._readstream(nml_file, nml_patch)
  File "C:\Users\jenkins\ESP_Python37\lib\site-packages\f90nml\parser.py", line 352, in _readstream
    self._update_tokens()
  File "C:\Users\jenkins\ESP_Python37\lib\site-packages\f90nml\parser.py", line 761, in _update_tokens
    next_token = next(self.tokens)
StopIteration
Premature exit in fun3dAIM preAnalysis status = -311
.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_3', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Warning: No boundary condition specified for capsGroup Wing2!
	Warning: No boundary condition specified for capsGroup Farfield!
	Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.

Using Python to write FUN3D namelist (fun3d.nml)
	fun3d.nml not found!
	Creating namelist
	Done writing nml file with Python

Getting CFD boundary conditions
	Boundary condition name - Wing1
	Warning: No boundary condition specified for capsGroup Wing2!
	Warning: No boundary condition specified for capsGroup Farfield!
	Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.

Using Python to write FUN3D namelist (fun3d.nml)

	Reading fun3d.nml .....
	Appending namelist
	Done writing nml file with Python

.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_4', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Python library was linked, but will not be used!
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Unrecognized "bcType" specified ("X") for Boundary_Condition tuple Wing1, current options (not all options are valid for this analysis tool - see AIM documentation) are " Inviscid, Viscous, Farfield, Extrapolate, Freestream, BackPressure, Symmetry, SubsonicInflow, SubsonicOutflow, MassflowIn, MassflowOut, MachOutflow, FixedInflow, FixedOutflow"
Premature exit in fun3dAIM preAnalysis status = -303
.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_5', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Python library was linked, but will not be used!
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Boundary condition name - X
	BC name "X" not found in attrMap
Premature exit in fun3dAIM preAnalysis status = -303
.
Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_6', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Python library was linked, but will not be used!
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Warning: No boundary condition specified for capsGroup Wing2!
	Warning: No boundary condition specified for capsGroup Farfield!
	Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
.Python library was linked, but will not be used!
Linking status during Attribute_Map = -303
Didn't find a link to Attribute_Map from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Boundary condition name - Farfield
	Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
Python library was linked, but will not be used!
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Boundary condition name - Farfield
	Done getting CFD boundary conditions
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Warning: The fun3d.nml file will be overwritten!
Writing fun3d.nml
.Analysis directory does not currently exist - it will be made automatically
 CAPS Info: No symbol for aimDiscr in aflr4AIM
 CAPS Info: No symbol for aimFreeDiscr in aflr4AIM
 CAPS Info: No symbol for aimLocateElement in aflr4AIM
 CAPS Info: No symbol for aimUsesDataSet in aflr4AIM
 CAPS Info: No symbol for aimCheck in aflr4AIM
 CAPS Info: No symbol for aimTransfer in aflr4AIM
 CAPS Info: No symbol for aimInterpolation in aflr4AIM
 CAPS Info: No symbol for aimInterpolateBar in aflr4AIM
 CAPS Info: No symbol for aimIntegration in aflr4AIM
 CAPS Info: No symbol for aimIntegrateBar in aflr4AIM
 CAPS Info: No symbol for aimSensitivity in aflr4AIM
 CAPS Info: No symbol for aimDiscr in aflr3AIM
 CAPS Info: No symbol for aimFreeDiscr in aflr3AIM
 CAPS Info: No symbol for aimLocateElement in aflr3AIM
 CAPS Info: No symbol for aimUsesDataSet in aflr3AIM
 CAPS Info: No symbol for aimCheck in aflr3AIM
 CAPS Info: No symbol for aimTransfer in aflr3AIM
 CAPS Info: No symbol for aimInterpolation in aflr3AIM
 CAPS Info: No symbol for aimInterpolateBar in aflr3AIM
 CAPS Info: No symbol for aimIntegration in aflr3AIM
 CAPS Info: No symbol for aimIntegrateBar in aflr3AIM
 CAPS Info: No symbol for aimSensitivity in aflr3AIM

Analysis object with the name, fun3dAIM, has already been initilized
('An altName of', 'fun3dAIM_7', 'will be used!')
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3

EGADS    : EGADS CAD Geometry Setup

EGADS    : Using EGADS Version 1.19
EGADS    : Using OpenCASCADE Version ase with OpenCASCADE 7.4.1

EGADS    : Model has 3 Bodies

EGADS    : Body 0 is a SolidBody
EGADS    : Body 0 has 1 BRep Shells
EGADS    : Body 0 has 8 BRep Faces
EGADS    : Body 0 has 15 BRep Edges
EGADS    : Body 0 has 9 BRep Nodes
EGADS    : Body 1 is a SolidBody
EGADS    : Body 1 has 1 BRep Shells
EGADS    : Body 1 has 8 BRep Faces
EGADS    : Body 1 has 15 BRep Edges
EGADS    : Body 1 has 9 BRep Nodes
EGADS    : Body 2 is a SolidBody
EGADS    : Body 2 has 1 BRep Shells
EGADS    : Body 2 has 2 BRep Faces
EGADS    : Body 2 has 6 BRep Edges
EGADS    : Body 2 has 2 BRep Nodes

AFLR4    : Surface Mesh Spacing Setup

AFLR4    : Max Bounding Box Length     = 160
AFLR4    : Min Bounding Box Length     = 160
AFLR4    : Max Ref Bounding Box Length = 14.1421
AFLR4    : Min Ref Bounding Box Length = 0.890888
AFLR4    : Reference Length            = 56.5685
AFLR4    : BL Thickness                = 0
AFLR4    : FarField Spacing            = 15.8264
AFLR4    : Abs Min Surf Spacing        = 0.141421
AFLR4    : Min Surf Spacing            = 0.282843
AFLR4    : Max Surf Spacing            = 5.65685

AFLR4    : Check Grid BCs

AFLR4    : Grid BCs are OK

AFLR4    : Geometry Definition Information

AFLR4    : IER = Isolated Edge Refinement
AFLR4    : ER  = Edge Refinement

AFLR4    : Definition         Definition  Composite             Grid BC       IER        ER     Scale
AFLR4    :         ID               Type         ID                Type      Flag    Weight    Factor
AFLR4    :          0 glue-only composite         -                   -         -         -         -
AFLR4    :          1        CAD geometry         0            STD w/BL         1         1         1
AFLR4    :          2        CAD geometry         0            STD w/BL         1         1         1
AFLR4    :          3        CAD geometry         0            STD w/BL         1         1         1
AFLR4    :          4        CAD geometry         0            STD w/BL         1         1         1
AFLR4    :          5        CAD geometry         0            STD w/BL         1         1         1
AFLR4    :          6        CAD geometry         0            STD w/BL         1         1         1
AFLR4    :          7        CAD geometry         0            STD w/BL         1         1         1
AFLR4    :          8        CAD geometry         0            STD w/BL         1         1         1
AFLR4    :          9        CAD geometry         0            STD w/BL         1         0        10
AFLR4    :         10        CAD geometry         0            STD w/BL         1         0        10
AFLR4    :         11        CAD geometry         0            STD w/BL         1         0        10
AFLR4    :         12        CAD geometry         0            STD w/BL         1         0        10
AFLR4    :         13        CAD geometry         0            STD w/BL         1         0        10
AFLR4    :         14        CAD geometry         0            STD w/BL         1         0        10
AFLR4    :         15        CAD geometry         0            STD w/BL         1         0        10
AFLR4    :         16        CAD geometry         0            STD w/BL         1         0        10
AFLR4    :         17        CAD geometry         0            FARFIELD         1         0         1
AFLR4    :         18        CAD geometry         0            FARFIELD         1         0         1

AFLR4    : Definition Neighbor Map

AFLR4    : Definition   Neighbor-Definitions
AFLR4    :          1   3 5 2 4
AFLR4    :          2   1 6 3 4
AFLR4    :          3   1 2 7 4
AFLR4    :          4   1 2 3
AFLR4    :          5   1 7 6 8
AFLR4    :          6   2 5 7 8
AFLR4    :          7   3 5 6 8
AFLR4    :          8   5 6 7
AFLR4    :          9   11 13 10 12
AFLR4    :         10   9 14 11 12
AFLR4    :         11   9 10 15 12
AFLR4    :         12   9 10 11
AFLR4    :         13   9 15 14 16
AFLR4    :         14   10 13 15 16
AFLR4    :         15   11 13 14 16
AFLR4    :         16   13 14 15
AFLR4    :         17   18
AFLR4    :         18   17

AFLR4    : Case has 2 Proximity Checking Components

AFLR4    : Component 1 includes...
           Definition 1 with ID/Label 1
           Definition 2 with ID/Label 2
           Definition 3 with ID/Label 3
           Definition 4 with ID/Label 4
           Definition 5 with ID/Label 5
           Definition 6 with ID/Label 6
           Definition 7 with ID/Label 7
           Definition 8 with ID/Label 8
AFLR4    : Component 2 includes...
           Definition 9 with ID/Label 9
           Definition 10 with ID/Label 10
           Definition 11 with ID/Label 11
           Definition 12 with ID/Label 12
           Definition 13 with ID/Label 13
           Definition 14 with ID/Label 14
           Definition 15 with ID/Label 15
           Definition 16 with ID/Label 16

AFLR4    : Define CAD surface definition 1
AFLR4    : Define CAD surface definition 2
AFLR4    : Define CAD surface definition 3
AFLR4    : Define CAD surface definition 4
AFLR4    : Define CAD surface definition 5
AFLR4    : Define CAD surface definition 6
AFLR4    : Define CAD surface definition 7
AFLR4    : Define CAD surface definition 8
AFLR4    : Define CAD surface definition 9
AFLR4    : Define CAD surface definition 10
AFLR4    : Define CAD surface definition 11
AFLR4    : Define CAD surface definition 12
AFLR4    : Define CAD surface definition 13
AFLR4    : Define CAD surface definition 14
AFLR4    : Define CAD surface definition 15
AFLR4    : Define CAD surface definition 16
AFLR4    : Define CAD surface definition 17
AFLR4    : Define CAD surface definition 18

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Faces      =       811      1487
AFLR4    : Nodes, Faces      =       662      1189

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Faces      =       808      1483
AFLR4    : Nodes, Faces      =       643      1153

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Faces      =       190       269
AFLR4    : Nodes, Faces      =       110       109

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Faces      =       182       282
AFLR4    : Nodes, Faces      =       182       282

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Faces      =       813      1491
AFLR4    : Nodes, Faces      =       662      1189

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Faces      =       804      1475
AFLR4    : Nodes, Faces      =       644      1155

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Faces      =       190       269
AFLR4    : Nodes, Faces      =       110       109

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Faces      =       182       282
AFLR4    : Nodes, Faces      =       182       282

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Faces      =       480       859
AFLR4    : Nodes, Faces      =       436       771

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Faces      =       331       561
AFLR4    : Nodes, Faces      =       431       761

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Faces      =       161       213
AFLR4    : Nodes, Faces      =       108       107

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Faces      =       181       280
AFLR4    : Nodes, Faces      =       180       278

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Faces      =       482       863
AFLR4    : Nodes, Faces      =       438       775

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Faces      =       290       479
AFLR4    : Nodes, Faces      =       442       783

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Faces      =       161       213
AFLR4    : Nodes, Faces      =       108       107

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Faces      =       181       280
AFLR4    : Nodes, Faces      =       180       278

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Faces      =        80       128
AFLR4    : Nodes, Faces      =       183       334

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Faces      =        80       128
AFLR4    : Nodes, Faces      =       182       332

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes, Faces      =      5003      9994

AFLR4    : Curvature BG Surface Grid Generation

AFLR4    : Nodes, Faces      =      5003      9994

AFLR4    : Surface Grid Generation

AFLR4    : Generate optimal mesh on surface definition 1
AFLR2    : Nodes, Faces      =       826      1503
AFLR4    : Nodes, Faces      =       811      1473

AFLR4    : Generate optimal mesh on surface definition 2
AFLR2    : Nodes, Faces      =       847      1545
AFLR4    : Nodes, Faces      =       785      1421

AFLR4    : Generate optimal mesh on surface definition 3
AFLR2    : Nodes, Faces      =       233       334
AFLR4    : Nodes, Faces      =       130       128

AFLR4    : Generate optimal mesh on surface definition 4
AFLR2    : Nodes, Faces      =       180       278
AFLR4    : Nodes, Faces      =       192       302

AFLR4    : Generate optimal mesh on surface definition 5
AFLR2    : Nodes, Faces      =       818      1487
AFLR4    : Nodes, Faces      =       814      1479

AFLR4    : Generate optimal mesh on surface definition 6
AFLR2    : Nodes, Faces      =       847      1545
AFLR4    : Nodes, Faces      =       786      1423

AFLR4    : Generate optimal mesh on surface definition 7
AFLR2    : Nodes, Faces      =       233       334
AFLR4    : Nodes, Faces      =       130       128

AFLR4    : Generate optimal mesh on surface definition 8
AFLR2    : Nodes, Faces      =       182       282
AFLR4    : Nodes, Faces      =       194       306

AFLR4    : Generate optimal mesh on surface definition 9
AFLR2    : Nodes, Faces      =       626      1142
AFLR4    : Nodes, Faces      =       608      1106

AFLR4    : Generate optimal mesh on surface definition 10
AFLR2    : Nodes, Faces      =       609      1108
AFLR4    : Nodes, Faces      =       597      1084

AFLR4    : Generate optimal mesh on surface definition 11
AFLR2    : Nodes, Faces      =       214       311
AFLR4    : Nodes, Faces      =       115       113

AFLR4    : Generate optimal mesh on surface definition 12
AFLR2    : Nodes, Faces      =       182       284
AFLR4    : Nodes, Faces      =       187       294

AFLR4    : Generate optimal mesh on surface definition 13
AFLR2    : Nodes, Faces      =       638      1165
AFLR4    : Nodes, Faces      =       614      1117

AFLR4    : Generate optimal mesh on surface definition 14
AFLR2    : Nodes, Faces      =       600      1090
AFLR4    : Nodes, Faces      =       599      1088

AFLR4    : Generate optimal mesh on surface definition 15
AFLR2    : Nodes, Faces      =       216       314
AFLR4    : Nodes, Faces      =       116       114

AFLR4    : Generate optimal mesh on surface definition 16
AFLR2    : Nodes, Faces      =       180       280
AFLR4    : Nodes, Faces      =       186       292

AFLR4    : Generate optimal mesh on surface definition 17
AFLR2    : Nodes, Faces      =        73       116
AFLR4    : Nodes, Faces      =       180       330

AFLR4    : Generate optimal mesh on surface definition 18
AFLR2    : Nodes, Faces      =        73       116
AFLR4    : Nodes, Faces      =       182       334

DGEOM    : Add surface definitions to composite definition 0
DGEOM    : Glue composite surface definition 0
DGEOM    : Nodes, Faces      =      6272     12532

AFLR4    : Proximity BG Surface Grid Generation

AFLR4    : Proximity BG Surface Grid Generation Skipped
AFLR4    : No Modifications Required

OVERALL  : CPU Time          =     0.401   seconds

AFLR4    : GET EGADS TESS FROM AFLR4 DATA

AFLR4    : EGADS TESS CREATED WITHOUT ERROR

AFLR4    : CHECK COORDINATES OF EGADS TESSELLATION

AFLR4    : CAD Definition=         1 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         2 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         3 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         4 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         5 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         6 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         7 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         8 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         1 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         2 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         3 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         4 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         5 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         6 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         7 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         8 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         1 Max Coordinate Deviation=0.000000e+00
AFLR4    : CAD Definition=         2 Max Coordinate Deviation=0.000000e+00

AFLR4    : COORDINATES OF EGADS TESSELLATION CHECKED WITHOUT ERROR

AFLR4    : CHECK AFLR4 AND EGADS TRIA-FACE ORDERING

AFLR4    : CAD Definition=         1 Ordering OK Reversed
AFLR4    : CAD Definition=         2 Ordering OK Reversed
AFLR4    : CAD Definition=         3 Ordering OK Reversed
AFLR4    : CAD Definition=         4 Ordering OK Reversed
AFLR4    : CAD Definition=         5 Ordering OK
AFLR4    : CAD Definition=         6 Ordering OK
AFLR4    : CAD Definition=         7 Ordering OK
AFLR4    : CAD Definition=         8 Ordering OK
AFLR4    : CAD Definition=         9 Ordering OK Reversed
AFLR4    : CAD Definition=        10 Ordering OK Reversed
AFLR4    : CAD Definition=        11 Ordering OK Reversed
AFLR4    : CAD Definition=        12 Ordering OK Reversed
AFLR4    : CAD Definition=        13 Ordering OK
AFLR4    : CAD Definition=        14 Ordering OK
AFLR4    : CAD Definition=        15 Ordering OK
AFLR4    : CAD Definition=        16 Ordering OK
AFLR4    : CAD Definition=        17 Ordering OK
AFLR4    : CAD Definition=        18 Ordering OK

AFLR4    : AFLR4 AND EGADS TRIA-FACE ORDERING CHECKED WITHOUT ERROR

Body = 1
Number of nodes = 3332
Number of elements = 6660
Number of tris = 6660
Number of quad = 0
Body = 2
Number of nodes = 2606
Number of elements = 5208
Number of tris = 5208
Number of quad = 0
Body = 3
Number of nodes = 334
Number of elements = 664
Number of tris = 664
Number of quad = 0
----------------------------
Total number of nodes = 6272
Total number of elements = 12532
Found link for groupMap (Attribute_Map) from parent
Mapping capsMesh attributes ................
	Number of unique capsMesh attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Found link for a surface mesh (Surface_Mesh) from parent
Number of surface nodes - 6272
Number of surface elements - 12532
Getting volume mesh
 
UG PARAM : SETTING INPUT PARAMETERS FROM ARGUMENT VECTOR
 
UG PARAM : mrecm                       = 2         
UG PARAM : mrecqm                      = 3         
 
AFLR3    : ---------------------------------------
AFLR3    : AFLR3 LIBRARY
AFLR3    : ADVANCING-FRONT/LOCAL-RECONNECTION
AFLR3    : TETRAHEDRAL GRID GENERATOR
AFLR3    : Version Number 16.30.16
AFLR3    : Version Date   10/10/20 @ 03:34PM
AFLR3    : Compile OS     CYGWIN_NT-6.1 2.10.0(0.325/5/3) x86_64
AFLR3    : Compile Date   10/11/20 @ 12:30PM
AFLR3    : Copyright 1994-2020, D.L. Marcum
AFLR3    : ---------------------------------------
 
AFLR3 IC : INPUT SURFACE GRID CHECK
 
AFLR3 IC : Nodes, Elements   =      6272         0
 
AFLR3    : CPU Time          =     0.015   seconds
 
AFLR3 IG : INITIAL VOLUME GRID GENERATION
 
AFLR3 IG : Nodes, Elements   =      6272         0
AFLR3 IG : Nodes, Elements   =         8        10
AFLR3 IG : Nodes, Elements   =      1256      7711
AFLR3 IG : Nodes, Elements   =      2512     16532
AFLR3 IG : Nodes, Elements   =      3768     25106
AFLR3 IG : Nodes, Elements   =      5024     34372
AFLR3 IG : Nodes, Elements   =      6279     43255
AFLR3 IG : Nodes, Elements   =      6279     43176
AFLR3 IG : Nodes, Elements   =      6279     43186
AFLR3 IG : Nodes, Elements   =      6279     43174
AFLR3 IG : Nodes, Elements   =      6279     43173
AFLR3 IG : Nodes, Elements   =      6272     25591
AFLR3 IG : Nodes, Elements   =      6272     25611
AFLR3 IG : Nodes, Elements   =      6272     20819
AFLR3 IG : Nodes, Elements   =      6272     18592
 
AFLR3    : CPU Time          =     0.241   seconds
 
AFLR3 GG : ISOTROPIC VOLUME GRID GENERATION
 
AFLR3 GG : Nodes, Elements   =      6272     18592
AFLR3 GG : Nodes, Elements   =      9124     27356
AFLR3 GG : Nodes, Elements   =      9124     39150
AFLR3 GG : Nodes, Elements   =      9124     36060
AFLR3 GG : Nodes, Elements   =      9124     34704
AFLR3 GG : Nodes, Elements   =     11611     42452
AFLR3 GG : Nodes, Elements   =     11611     53246
AFLR3 GG : Nodes, Elements   =     11611     49980
AFLR3 GG : Nodes, Elements   =     11611     48992
AFLR3 GG : Nodes, Elements   =     14415     57628
AFLR3 GG : Nodes, Elements   =     14415     70628
AFLR3 GG : Nodes, Elements   =     14415     66640
AFLR3 GG : Nodes, Elements   =     14415     65506
AFLR3 GG : Nodes, Elements   =     17320     74389
AFLR3 GG : Nodes, Elements   =     17320     87667
AFLR3 GG : Nodes, Elements   =     17320     83529
AFLR3 GG : Nodes, Elements   =     17320     82504
AFLR3 GG : Nodes, Elements   =     20360     91794
AFLR3 GG : Nodes, Elements   =     20360    105676
AFLR3 GG : Nodes, Elements   =     20360    101509
AFLR3 GG : Nodes, Elements   =     20360    100433
AFLR3 GG : Nodes, Elements   =     23495    109961
AFLR3 GG : Nodes, Elements   =     23495    124295
AFLR3 GG : Nodes, Elements   =     23495    119966
AFLR3 GG : Nodes, Elements   =     23495    118854
AFLR3 GG : Nodes, Elements   =     26822    128955
AFLR3 GG : Nodes, Elements   =     26822    144091
AFLR3 GG : Nodes, Elements   =     26822    139613
AFLR3 GG : Nodes, Elements   =     26822    138473
AFLR3 GG : Nodes, Elements   =     30208    148734
AFLR3 GG : Nodes, Elements   =     30208    164124
AFLR3 GG : Nodes, Elements   =     30208    159530
AFLR3 GG : Nodes, Elements   =     30208    158421
AFLR3 GG : Nodes, Elements   =     33756    169164
AFLR3 GG : Nodes, Elements   =     33756    185021
AFLR3 GG : Nodes, Elements   =     33756    180387
AFLR3 GG : Nodes, Elements   =     33756    179298
AFLR3 GG : Nodes, Elements   =     37335    190116
AFLR3 GG : Nodes, Elements   =     37335    206268
AFLR3 GG : Nodes, Elements   =     37335    201512
AFLR3 GG : Nodes, Elements   =     37335    200436
AFLR3 GG : Nodes, Elements   =     40937    211291
AFLR3 GG : Nodes, Elements   =     40937    227435
AFLR3 GG : Nodes, Elements   =     40937    222741
AFLR3 GG : Nodes, Elements   =     40937    221698
AFLR3 GG : Nodes, Elements   =     44599    232725
AFLR3 GG : Nodes, Elements   =     44599    248966
AFLR3 GG : Nodes, Elements   =     44599    244350
AFLR3 GG : Nodes, Elements   =     44599    243297
AFLR3 GG : Nodes, Elements   =     48110    253870
AFLR3 GG : Nodes, Elements   =     48110    269496
AFLR3 GG : Nodes, Elements   =     48110    265109
AFLR3 GG : Nodes, Elements   =     48110    264155
AFLR3 GG : Nodes, Elements   =     51559    274523
AFLR3 GG : Nodes, Elements   =     51559    290017
AFLR3 GG : Nodes, Elements   =     51559    285528
AFLR3 GG : Nodes, Elements   =     51559    284657
AFLR3 GG : Nodes, Elements   =     54954    294863
AFLR3 GG : Nodes, Elements   =     54954    310064
AFLR3 GG : Nodes, Elements   =     54954    305791
AFLR3 GG : Nodes, Elements   =     54954    304943
AFLR3 GG : Nodes, Elements   =     58183    314640
AFLR3 GG : Nodes, Elements   =     58183    328708
AFLR3 GG : Nodes, Elements   =     58183    324892
AFLR3 GG : Nodes, Elements   =     58183    324175
AFLR3 GG : Nodes, Elements   =     61258    333411
AFLR3 GG : Nodes, Elements   =     61258    346914
AFLR3 GG : Nodes, Elements   =     61258    343177
AFLR3 GG : Nodes, Elements   =     61258    342501
AFLR3 GG : Nodes, Elements   =     64088    350998
AFLR3 GG : Nodes, Elements   =     64088    363320
AFLR3 GG : Nodes, Elements   =     64088    359947
AFLR3 GG : Nodes, Elements   =     64088    359363
AFLR3 GG : Nodes, Elements   =     66690    367171
AFLR3 GG : Nodes, Elements   =     66690    378470
AFLR3 GG : Nodes, Elements   =     66690    375464
AFLR3 GG : Nodes, Elements   =     66690    374960
AFLR3 GG : Nodes, Elements   =     68981    381838
AFLR3 GG : Nodes, Elements   =     68981    391895
AFLR3 GG : Nodes, Elements   =     68981    389087
AFLR3 GG : Nodes, Elements   =     68981    388655
AFLR3 GG : Nodes, Elements   =     70925    394488
AFLR3 GG : Nodes, Elements   =     70925    403216
AFLR3 GG : Nodes, Elements   =     70925    400695
AFLR3 GG : Nodes, Elements   =     70925    400378
AFLR3 GG : Nodes, Elements   =     72425    404880
AFLR3 GG : Nodes, Elements   =     72425    411639
AFLR3 GG : Nodes, Elements   =     72425    409610
AFLR3 GG : Nodes, Elements   =     72425    409388
AFLR3 GG : Nodes, Elements   =     73580    412860
AFLR3 GG : Nodes, Elements   =     73580    417987
AFLR3 GG : Nodes, Elements   =     73580    416568
AFLR3 GG : Nodes, Elements   =     73580    416392
AFLR3 GG : Nodes, Elements   =     74452    419008
AFLR3 GG : Nodes, Elements   =     74452    422765
AFLR3 GG : Nodes, Elements   =     74452    421708
AFLR3 GG : Nodes, Elements   =     74452    421574
AFLR3 GG : Nodes, Elements   =     75021    423281
AFLR3 GG : Nodes, Elements   =     75021    425902
AFLR3 GG : Nodes, Elements   =     75021    425089
AFLR3 GG : Nodes, Elements   =     75021    425022
AFLR3 GG : Nodes, Elements   =     75376    426088
AFLR3 GG : Nodes, Elements   =     75376    427675
AFLR3 GG : Nodes, Elements   =     75376    427188
AFLR3 GG : Nodes, Elements   =     75376    427142
AFLR3 GG : Nodes, Elements   =     75562    427700
AFLR3 GG : Nodes, Elements   =     75562    428537
AFLR3 GG : Nodes, Elements   =     75562    428267
AFLR3 GG : Nodes, Elements   =     75562    428235
AFLR3 GG : Nodes, Elements   =     75654    428511
AFLR3 GG : Nodes, Elements   =     75654    428923
AFLR3 GG : Nodes, Elements   =     75654    428783
AFLR3 GG : Nodes, Elements   =     75654    428776
AFLR3 GG : Nodes, Elements   =     75690    428884
AFLR3 GG : Nodes, Elements   =     75690    429039
AFLR3 GG : Nodes, Elements   =     75690    428980
AFLR3 GG : Nodes, Elements   =     75690    428973
AFLR3 GG : Nodes, Elements   =     75703    429012
AFLR3 GG : Nodes, Elements   =     75703    429065
AFLR3 GG : Nodes, Elements   =     75703    429045
AFLR3 GG : Nodes, Elements   =     75703    429043
AFLR3 GG : Nodes, Elements   =     75812    429370
AFLR3 GG : Nodes, Elements   =     75812    429807
AFLR3 GG : Nodes, Elements   =     75812    429638
AFLR3 GG : Nodes, Elements   =     75812    429620
AFLR3 GG : Nodes, Elements   =     75834    429686
AFLR3 GG : Nodes, Elements   =     75834    429783
AFLR3 GG : Nodes, Elements   =     75834    429742
AFLR3 GG : Nodes, Elements   =     75834    429736
AFLR3 GG : Nodes, Elements   =     75843    429763
AFLR3 GG : Nodes, Elements   =     75843    429799
AFLR3 GG : Nodes, Elements   =     75843    429789
AFLR3 GG : Nodes, Elements   =     75843    429786
AFLR3 GG : Nodes, Elements   =     75847    429798
AFLR3 GG : Nodes, Elements   =     75847    429818
AFLR3 GG : Nodes, Elements   =     75847    429811
AFLR3 GG : Nodes, Elements   =     75847    429809
AFLR3 GG : Nodes, Elements   =     75848    429812
AFLR3 GG : Nodes, Elements   =     75848    429818
AFLR3 GG : Nodes, Elements   =     75848    429815
AFLR3 GG : Nodes, Elements   =     75849    429818
AFLR3 GG : Nodes, Elements   =     75849    429824
AFLR3 GG : Nodes, Elements   =     75849    429821
AFLR3 GG : Nodes, Elements   =     75850    429824
AFLR3 GG : Nodes, Elements   =     75850    429826
 
AFLR3    : CPU Time          =    15.889   seconds
 
AFLR3 QI : QUALITY IMPROVEMENT
 
AFLR3 QI : Nodes, Elements   =     75850    429826
AFLR3 QI : Nodes, Elements   =     73454    416572
AFLR3 QI : Nodes, Elements   =     72903    413515
AFLR3 QI : Nodes, Elements   =     72861    413273
AFLR3 QI : Nodes, Elements   =     72860    413268
AFLR3 QI : Nodes, Elements   =     72860    419763
AFLR3 QI : Nodes, Elements   =     72860    413293
AFLR3 QI : Nodes, Elements   =     72860    412270
AFLR3 QI : Nodes, Elements   =     72860    415246
AFLR3 QI : Nodes, Elements   =     72860    412294
AFLR3 QI : Nodes, Elements   =     72860    412205
AFLR3 QI : Nodes, Elements   =     72860    412862
AFLR3 QI : Nodes, Elements   =     72860    412099
AFLR3 QI : Nodes, Elements   =     72860    411970
AFLR3 QI : Nodes, Elements   =     72860    412317
AFLR3 QI : Nodes, Elements   =     72860    411937
AFLR3 QI : Nodes, Elements   =     72860    411862
AFLR3 QI : Nodes, Elements   =     72860    412153
AFLR3 QI : Nodes, Elements   =     72860    411848
AFLR3 QI : Nodes, Elements   =     72860    411798
AFLR3 QI : Nodes, Elements   =     72868    411836
AFLR3 QI : Nodes, Elements   =     72868    412127
AFLR3 QI : Nodes, Elements   =     72868    411846
AFLR3 QI : Nodes, Elements   =     72868    411834
AFLR3 QI : Nodes, Elements   =     72868    412109
AFLR3 QI : Nodes, Elements   =     72868    411837
AFLR3 QI : Nodes, Elements   =     72868    411802
AFLR3 QI : Nodes, Elements   =     72868    411836
 
AFLR3    : CPU Time          =     4.684   seconds
 
AFLR3 QRG: QUALITY GRID RE-GENERATION
 
AFLR3 QRG: Nodes, Elements   =     72868    411836
AFLR3 QRG: Nodes, Elements   =     72884    411920
AFLR3 QRG: Nodes, Elements   =     72885    411925
 
AFLR3    : CPU Time          =     0.212   seconds
 
AFLR3    : DONE

UG3      : DIHEDRAL ANGLE CHECK

UG3      : No. Tet Elems     =    411925
UG3      : Min, Max Ang      =    0.9437     176.6
UG3      : Average Angle     =      70.2
UG3      : No. Angle>160.0   =        75
UG3      : No. Angle>179.9   =         0

UG3      : VOL CHECK

UG3      : Total-Volume      = 2.11e+006

UG3      : No. Tet Elems     =    411925
UG3      : Min Vol           = 5.82e-010
UG3      : Average Vol       =      5.12
UG3      : Total-Tet-Vol     = 2.11e+006
UG3      : No. Vol<TOL       =         0

UG3      : Q VOL-LENGTH-RATIO CHECK
                      2/3        2
UG3      : Q = c * Vol   / sum( L  )
UG3      : 0 <= Q <= 1

UG3      : No. Tet Elems     =    411925
UG3      : Min, Max Q        =    0.0604         1
UG3      : Average Q         =      0.89
UG3      : No. Q<       0.1  =        22
UG3      : No. Q<      0.01  =         0
Volume mesh:
	Number of nodes = 72885
	Number of elements = 424457
	Number of triangles = 12532
	Number of quadrilatarals = 0
	Number of tetrahedrals = 411925
	Number of pyramids= 0
	Number of prisms= 0
	Number of hexahedrals= 0
No project name ("Proj_Name") provided - A volume mesh will not be written out
Python library was linked, but will not be used!
Found link for attrMap (Attribute_Map) from parent
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Boundary condition name - Farfield
	Done getting CFD boundary conditions

Getting CFD design variables.......
	Number of design variables - 1
	Design Variable name - Alpha
	Done getting CFD design variables
Getting CFD objective.......
	Number of design variables - 1
	Objective name - ClCd
	Done getting CFD objective
Found link for volume mesh (Volume_Mesh) from parent

Writing AFLR3 file ....
Finished writing AFLR3 file


Writing MAPBC file ....
Finished writing MAPBC file

Since Python was not linked and/or being used, the "Overwrite_NML" input needs to be set to "True" to give permission to create a new fun3d.nml. fun3d.nml will NOT be updated!!
No recognized data transfer names found!
Error: Premature exit in fun3d_dataTransfer status = -303
Creating FUN3D directory tree
Writing sensitivity file for body 1, File - Rubberize\model.tec.1.sd1
Writing sensitivity file for body 2, File - Rubberize\model.tec.2.sd1
Writing sensitivity file for body 3, File - Rubberize\model.tec.3.sd1
Writing rubber.data 
. Cleaning up fun3dInstance - 0
 Cleaning up fun3dInstance - 1
 Cleaning up fun3dInstance - 2
 Cleaning up fun3dInstance - 3
 Cleaning up fun3dInstance - 4
 Cleaning up fun3dInstance - 5
 Cleaning up fun3dInstance - 6
 Cleaning up fun3dInstance - 7
 Cleaning up aflr4Instance - 0
 Cleaning up aflr3Instance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 2659) at Close!
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
No analysis directory provided - defaulting to current working directory
 CAPS Info: No symbol for aimDiscr in masstranAIM
 CAPS Info: No symbol for aimFreeDiscr in masstranAIM
 CAPS Info: No symbol for aimLocateElement in masstranAIM
 CAPS Info: No symbol for aimUsesDataSet in masstranAIM
 CAPS Info: No symbol for aimCheck in masstranAIM
 CAPS Info: No symbol for aimTransfer in masstranAIM
 CAPS Info: No symbol for aimInterpolation in masstranAIM
 CAPS Info: No symbol for aimInterpolateBar in masstranAIM
 CAPS Info: No symbol for aimIntegration in masstranAIM
 CAPS Info: No symbol for aimIntegrateBar in masstranAIM
 CAPS Info: No symbol for aimData in masstranAIM
 CAPS Info: No symbol for aimSensitivity in masstranAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] ifthen:             0.00000  EQ      1.00000  and  ...
    executing [   5] ifthen:             1.00000  EQ      1.00000  and      0.00000  eq      0.00000
    executing [   6] box:            0.00000      0.00000      0.00000      1.00000      1.00000      1.00000
                          Body      1 created  (toler= 1.0000e-07, nnode=   8, nedge=  12, nface=   6)
    executing [   7] select:   body  1
                    putting Branch Attributes on Body
    executing [   9] ifthen:             0.00000  EQ      1.00000  and  ...
    executing [  16] ifthen:             0.00000  EQ      1.00000  and  ...
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    box                       1       0.003   50.0
    select                    1       0.001   16.7
    ifthen                    4       0.002   33.3
    endif                     4       0.000    0.0
    Total                    10       0.006
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Didn't find a Surface mesh (Surface_Mesh) from parent - checking for volume mesh
Didn't find a volume mesh (Volume_Mesh) from parent
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
 EGADS Info: 0 Objects, 0 Reference in Use (of 135) at Close!
.Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
No analysis directory provided - defaulting to current working directory
 CAPS Info: No symbol for aimDiscr in masstranAIM
 CAPS Info: No symbol for aimFreeDiscr in masstranAIM
 CAPS Info: No symbol for aimLocateElement in masstranAIM
 CAPS Info: No symbol for aimUsesDataSet in masstranAIM
 CAPS Info: No symbol for aimCheck in masstranAIM
 CAPS Info: No symbol for aimTransfer in masstranAIM
 CAPS Info: No symbol for aimInterpolation in masstranAIM
 CAPS Info: No symbol for aimInterpolateBar in masstranAIM
 CAPS Info: No symbol for aimIntegration in masstranAIM
 CAPS Info: No symbol for aimIntegrateBar in masstranAIM
 CAPS Info: No symbol for aimData in masstranAIM
 CAPS Info: No symbol for aimSensitivity in masstranAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] ifthen:             0.00000  EQ      1.00000  and  ...
    executing [   5] ifthen:             0.00000  EQ      1.00000  and  ...
    executing [   9] ifthen:             1.00000  EQ      1.00000  and      0.00000  eq      0.00000
    executing [  10] box:            2.00000      0.00000      0.00000      1.00000      1.00000      1.00000
                          Body      1 created  (toler= 1.0000e-07, nnode=   8, nedge=  12, nface=   6)
    executing [  11] select:   face  1
                     putting Branch Attributes on Face 1
    executing [  12] select:   face  3
                     putting Branch Attributes on Face 3
    executing [  13] select:   face  6
                     putting Branch Attributes on Face 6
    executing [  14] select:   body  1
                    putting Branch Attributes on Body
    executing [  16] ifthen:             0.00000  EQ      1.00000  and  ...
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    box                       1       0.004   50.0
    select                    4       0.003   37.5
    ifthen                    4       0.001   12.5
    endif                     4       0.000    0.0
    Total                    13       0.008
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Didn't find a Surface mesh (Surface_Mesh) from parent - checking for volume mesh
Didn't find a volume mesh (Volume_Mesh) from parent
Creating FEA BEM
	Face 3 quading disabled with attribute .qParams
	Face 6 quading disabled with attribute .qParams
	Getting quads for BEM!
	capsIgnore attribute found for face - 1!!
Removing unused nodes...
	Removed 324 (out of 4009) unused nodes!
	Mesh for body = 0
	Number of nodal coordinates = 3685
	Number of elements = 6209
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 5126
	Elemental Quad4 = 1083

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
 EGADS Info: 0 Objects, 0 Reference in Use (of 135) at Close!
.Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
No analysis directory provided - defaulting to current working directory
 CAPS Info: No symbol for aimDiscr in masstranAIM
 CAPS Info: No symbol for aimFreeDiscr in masstranAIM
 CAPS Info: No symbol for aimLocateElement in masstranAIM
 CAPS Info: No symbol for aimUsesDataSet in masstranAIM
 CAPS Info: No symbol for aimCheck in masstranAIM
 CAPS Info: No symbol for aimTransfer in masstranAIM
 CAPS Info: No symbol for aimInterpolation in masstranAIM
 CAPS Info: No symbol for aimInterpolateBar in masstranAIM
 CAPS Info: No symbol for aimIntegration in masstranAIM
 CAPS Info: No symbol for aimIntegrateBar in masstranAIM
 CAPS Info: No symbol for aimData in masstranAIM
 CAPS Info: No symbol for aimSensitivity in masstranAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] ifthen:             0.00000  EQ      1.00000  and  ...
    executing [   5] ifthen:             0.00000  EQ      1.00000  and  ...
    executing [   9] ifthen:             0.00000  EQ      1.00000  and  ...
    executing [  16] ifthen:             1.00000  EQ      1.00000  and      0.00000  eq      0.00000
    executing [  17] box:            4.00000      0.00000      0.00000      1.00000      1.00000      1.00000
                          Body      1 created  (toler= 1.0000e-07, nnode=   8, nedge=  12, nface=   6)
    executing [  18] select:   face  1
                     putting Branch Attributes on Face 1
    executing [  19] select:   face  2
                     putting Branch Attributes on Face 2
    executing [  20] select:   face  3
                     putting Branch Attributes on Face 3
    executing [  21] select:   face  4
                     putting Branch Attributes on Face 4
    executing [  22] select:   face  5
                     putting Branch Attributes on Face 5
    executing [  23] select:   face  6
                     putting Branch Attributes on Face 6
    executing [  24] select:   body  1
                    putting Branch Attributes on Body
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    box                       1       0.003   60.0
    select                    7       0.001   20.0
    ifthen                    4       0.001   20.0
    endif                     4       0.000    0.0
    Total                    16       0.005
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = box1, index = 1
	Name = box2, index = 2
Didn't find a Surface mesh (Surface_Mesh) from parent - checking for volume mesh
Didn't find a volume mesh (Volume_Mesh) from parent
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 2168
	Number of elements = 2166
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 2166

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 2
	Property name - box1
	Property name - box2
	Done getting FEA properties
Updating mesh element types based on properties input
 EGADS Info: 0 Objects, 0 Reference in Use (of 135) at Close!
.Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
No analysis directory provided - defaulting to current working directory
 CAPS Info: No symbol for aimDiscr in masstranAIM
 CAPS Info: No symbol for aimFreeDiscr in masstranAIM
 CAPS Info: No symbol for aimLocateElement in masstranAIM
 CAPS Info: No symbol for aimUsesDataSet in masstranAIM
 CAPS Info: No symbol for aimCheck in masstranAIM
 CAPS Info: No symbol for aimTransfer in masstranAIM
 CAPS Info: No symbol for aimInterpolation in masstranAIM
 CAPS Info: No symbol for aimInterpolateBar in masstranAIM
 CAPS Info: No symbol for aimIntegration in masstranAIM
 CAPS Info: No symbol for aimIntegrateBar in masstranAIM
 CAPS Info: No symbol for aimData in masstranAIM
 CAPS Info: No symbol for aimSensitivity in masstranAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] ifthen:             1.00000  EQ      1.00000  and      0.00000  eq      0.00000
    executing [   2] box:            0.00000      0.00000      0.00000      2.00000      3.00000      0.00000
                          Body      1 created  (toler= 1.0000e-07, nnode=   4, nedge=   4, nface=   1)
    executing [   3] select:   body  1
                    putting Branch Attributes on Body
    executing [   5] ifthen:             0.00000  EQ      1.00000  and  ...
    executing [   9] ifthen:             0.00000  EQ      1.00000  and  ...
    executing [  16] ifthen:             0.00000  EQ      1.00000  and  ...
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    box                       1       0.003   42.9
    select                    1       0.001   14.3
    ifthen                    4       0.003   42.9
    endif                     4       0.000    0.0
    Total                    10       0.007
Mapping Csys attributes ................
	Number of unique Csys attributes = 0

Getting FEA coordinate systems.......
	Number of coordinate systems - 0
	No coordinate systems found - defaulting to global
Mapping capsConstraint attributes ................
	Number of unique capsConstraint attributes = 0
Mapping capsLoad attributes ................
	Number of unique capsLoad attributes = 0
Mapping capsBound attributes ................
	Number of unique capsBound attributes = 0
Mapping capsConnect attributes ................
	Number of unique capsConnect attributes = 0
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = box1, index = 1
Didn't find a Surface mesh (Surface_Mesh) from parent - checking for volume mesh
Didn't find a volume mesh (Volume_Mesh) from parent
Creating FEA BEM
	Getting quads for BEM!
	Mesh for body = 0
	Number of nodal coordinates = 400
	Number of elements = 361
	Elemental Nodes = 0
	Elemental Rods  = 0
	Elemental Tria3 = 0
	Elemental Quad4 = 361

Getting FEA materials.......
	Number of materials - 2
	Material name - madeupium
	Material name - unobtainium
	Done getting FEA materials

Getting FEA properties.......
	Number of properties - 1
	Property name - box1
	Done getting FEA properties
Updating mesh element types based on properties input
 EGADS Info: 0 Objects, 0 Reference in Use (of 80) at Close!
.Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
ssssssssss EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
Analysis directory does not currently exist - it will be made automatically
 CAPS Info: No symbol for aimExecute in su2AIM
 CAPS Info: No symbol for aimCheck in su2AIM
 CAPS Info: No symbol for aimData in su2AIM
 CAPS Info: No symbol for aimSensitivity in su2AIM

Analysis object with the name, su2AIM, has already been initilized
('An altName of', 'su2AIM_1', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] set:            cmean  sqrt(area/aspect)
                          cmean =     2.82843     0.00000
    executing [   2] set:            span  cmean*aspect
                          span =    14.14214     0.00000
    executing [   3] set:            sspan  span/2
                          sspan =     7.07107     0.00000
    executing [   4] set:            croot  2*cmean/(1+taper)
                          croot =     3.77124     0.00000
    executing [   5] set:            ctip  croot*taper
                          ctip =     1.88562     0.00000
    executing [   6] set:            xtip  sspan*tand(lesweep)
                          xtip =     4.08248     0.00000
    executing [   7] set:            ytip  sspan*tand(dihedral)
                          ytip =     0.12343     0.00000
    executing [   8] set:            ybot  -0.1*croot
                          ybot =    -0.37712     0.00000
    executing [   9] set:            ytop  +0.2*croot+ytip
                          ytop =     0.87767     0.00000
    executing [  10] set:            extend  0.02*cmean
                          extend =     0.05657     0.00000
    executing [  11] mark:
                          Mark        created
    executing [  12] udprim:     naca Series  8412.00000 (compiled code)
                          Body      1 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  13] scale:          3.77124      0.00000      0.00000      0.00000
                          Body      2 created  (toler= 3.7712e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  14] udprim:     naca Series    20.00000 (compiled code)
                          Body      3 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  15] scale:          1.88562      0.00000      0.00000      0.00000
                          Body      4 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  16] rotatez:      -15.00000      0.00000      0.00000
                          Body      5 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  17] translate:      4.08248      0.12343     -7.07107
                          Body      6 created  (toler= 1.8856e-07, nnode=   3, nedge=   3, nface=   1)
    executing [  18] rule:           0.00000      0.00000
                          ruling  2 Xsects with 3 Strips each...
                          Body      7 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  19] store:      HalfWing      0.00000      0.00000
                          Body      7 stored
    executing [  20] restore:    HalfWing      0.00000
                          Body      8 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  21] restore:    HalfWing      0.00000
                          Body      9 restored (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  22] mirror:         0.00000      0.00000      1.00000      0.00000
                          Body     10 created  (toler= 1.0000e-07, nnode=   6, nedge=   9, nface=   5)
    executing [  23] join:           0.00000      0.00000
                          Body     11 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  24] rotatex:       90.00000      0.00000      0.00000
                          Body     12 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  25] store:      Wing      0.00000      0.00000
                          Body     12 stored
    executing [  26] restore:    Wing      0.00000
                          Body     13 restored (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  27] restore:    Wing      0.00000
                          Body     14 restored (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  28] scale:          0.40000      0.00000      0.00000      0.00000
                          Body     15 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  29] translate:     10.00000      0.00000      0.00000
                          Body     16 created  (toler= 1.0000e-07, nnode=   9, nedge=  15, nface=   8)
    executing [  30] sphere:         0.00000      0.00000      0.00000     80.00000
                          Body     17 created  (toler= 1.0000e-05, nnode=   2, nedge=   6, nface=   2)
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    sphere                    1       0.005    0.6
    udprim                    2       0.029    3.2
    restore                   4       0.023    2.6
    rule                      1       0.124   13.9
    join                      1       0.149   16.7
    translate                 2       0.123   13.8
    rotatex                   1       0.152   17.0
    rotatez                   1       0.002    0.2
    scale                     3       0.235   26.3
    mirror                    1       0.046    5.2
    set                      10       0.004    0.4
    store                     2       0.000    0.0
    mark                      1       0.001    0.1
    Total                    30       0.893
Linking status during attrMap (Attribute_Map) = -303
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Unrecognized "bcType" specified ("X") for Boundary_Condition tuple Wing1, current options (not all options are valid for this analysis tool - see AIM documentation) are " Inviscid, Viscous, Farfield, Extrapolate, Freestream, BackPressure, Symmetry, SubsonicInflow, SubsonicOutflow, MassflowIn, MassflowOut, MachOutflow, FixedInflow, FixedOutflow"
Premature exit in su2AIM preAnalysis status = -303
.
Analysis object with the name, su2AIM, has already been initilized
('An altName of', 'su2AIM_2', 'will be used!')
Analysis directory does not currently exist - it will be made automatically
Linking status during attrMap (Attribute_Map) = -303
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Boundary condition name - X
	BC name "X" not found in attrMap
Premature exit in su2AIM preAnalysis status = -303
.Linking status during attrMap (Attribute_Map) = -303
Didn't find a link to attrMap from parent - getting it ourselves
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Farfield, index = 3
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Boundary condition name - Farfield
	Done getting CFD boundary conditions
Linking status = -303
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.0.7) "
Getting CFD boundary conditions
	Boundary condition name - Wing1
	Boundary condition name - Wing2
	Boundary condition name - Farfield
	Done getting CFD boundary conditions
Linking status = -303
Didn't find a link to a volume mesh (Volume_Mesh) from parent - a volume mesh will NOT be created.
Warning: The su2 cfg file will be overwritten!
Write SU2 configuration file for version "BlackBird (7.0.7) "
. Cleaning up su2Instance - 0
 Cleaning up su2Instance - 1
 Cleaning up su2Instance - 2
 EGADS Info: 0 Objects, 0 Reference in Use (of 2134) at Close!
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
Analysis directory does not currently exist - it will be made automatically
 CAPS Info: No symbol for aimDiscr in xfoilAIM
 CAPS Info: No symbol for aimFreeDiscr in xfoilAIM
 CAPS Info: No symbol for aimLocateElement in xfoilAIM
 CAPS Info: No symbol for aimUsesDataSet in xfoilAIM
 CAPS Info: No symbol for aimExecute in xfoilAIM
 CAPS Info: No symbol for aimCheck in xfoilAIM
 CAPS Info: No symbol for aimTransfer in xfoilAIM
 CAPS Info: No symbol for aimInterpolation in xfoilAIM
 CAPS Info: No symbol for aimInterpolateBar in xfoilAIM
 CAPS Info: No symbol for aimIntegration in xfoilAIM
 CAPS Info: No symbol for aimIntegrateBar in xfoilAIM
 CAPS Info: No symbol for aimData in xfoilAIM
 CAPS Info: No symbol for aimSensitivity in xfoilAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] dimension:     classvar      1.00000      2.00000
    executing [   2] dimension:     ztailvar      1.00000      2.00000
    executing [   3] dimension:     auppervar      1.00000      4.00000
    executing [   4] dimension:     alowervar      1.00000      4.00000
    executing [   5] set:            classvar  0.5;1.0;
                          classvar[1,1] =     0.50000     0.00000
                          classvar[1,2] =     1.00000     0.00000
    executing [   6] set:            ztailvar  0.001;-0.001;
                          ztailvar[1,1] =     0.00100     0.00000
                          ztailvar[1,2] =    -0.00100     0.00000
    executing [   7] set:            al4  0.001
                          al4 =     0.00100     0.00000
    executing [   8] set:            auppervar  au1;au2;au3;au4;
                          auppervar[1,1] =     0.22000     0.00000
                          auppervar[1,2] =     0.30000     0.00000
                          auppervar[1,3] =     0.25000     0.00000
                          auppervar[1,4] =     0.29000     0.00000
    executing [   9] set:            alowervar  al1;al2;al3;al4;
                          alowervar[1,1] =    -0.12000     0.00000
                          alowervar[1,2] =    -0.02000     0.00000
                          alowervar[1,3] =    -0.03000     0.00000
                          alowervar[1,4] =     0.00100     0.00000
    executing [  10] udparg:     kulfan class     0.50000 
                          Body      1 created  (NULL Body)
    executing [  11] udparg:     kulfan ztail     0.00100 
                          Body      2 created  (NULL Body)
    executing [  12] udparg:     kulfan aupper     0.22000 
                          Body      3 created  (NULL Body)
    executing [  13] udparg:     kulfan alower    -0.12000 
                          Body      4 created  (NULL Body)
    executing [  14] udprim:     kulfan (compiled code)
                          Body      5 created  (toler= 1.0000e-07, nnode=   3, nedge=   3, nface=   1)
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    dimension                 4       0.001    2.3
    udprim                    1       0.034   77.3
    set                       5       0.006   13.6
    udparg                    4       0.003    6.8
    Total                    14       0.044


Running xFoil......
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL
.

Running xFoil......
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL
. EGADS Info: 0 Objects, 0 Reference in Use (of 91) at Close!
Definition of "kt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 90, overrides prefixed-unit "1000000 kilogram"
Definition of "microns" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 336, overrides prefixed-unit "1e-15 second"
Definition of "ft" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 433, overrides prefixed-unit "1e-12 kilogram"
Definition of "yd" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 441, overrides prefixed-unit "8.64e-20 second"
Definition of "pt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 655, overrides prefixed-unit "1e-09 kilogram"
Definition of "at" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1052, overrides prefixed-unit "1e-15 kilogram"
Definition of "ph" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1571, overrides prefixed-unit "3.6e-09 second"
Definition of "nt" in "\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\udunits\/udunits2-common.xml", line 1578, overrides prefixed-unit "1e-06 kilogram"
--> enter ocsmCheck()
--> checks passed
--> enter ocsmSave(filename=capsTmp.cpc)
--> enter ocsmCheck()
--> checks passed
Analysis directory does not currently exist - it will be made automatically
 CAPS Info: No symbol for aimDiscr in xfoilAIM
 CAPS Info: No symbol for aimFreeDiscr in xfoilAIM
 CAPS Info: No symbol for aimLocateElement in xfoilAIM
 CAPS Info: No symbol for aimUsesDataSet in xfoilAIM
 CAPS Info: No symbol for aimExecute in xfoilAIM
 CAPS Info: No symbol for aimCheck in xfoilAIM
 CAPS Info: No symbol for aimTransfer in xfoilAIM
 CAPS Info: No symbol for aimInterpolation in xfoilAIM
 CAPS Info: No symbol for aimInterpolateBar in xfoilAIM
 CAPS Info: No symbol for aimIntegration in xfoilAIM
 CAPS Info: No symbol for aimIntegrateBar in xfoilAIM
 CAPS Info: No symbol for aimData in xfoilAIM
 CAPS Info: No symbol for aimSensitivity in xfoilAIM
--> enter ocsmBuild(buildTo=0)
--> enter ocsmCheck()
--> checks passed

    Interim EGADS version  1.19 (with  OpenCASCADE 7.4.1)

    executing [   1] udprim:     naca Thickness     0.12000 Camber     0.02000 sharpte     1.00000 (compiled code)
                          Body      1 created  (toler= 1.0000e-07, nnode=   2, nedge=   2, nface=   1)
    finalizing:
==> Profile information
    Branch type           ncall  time (sec)    pct
    udprim                    1       0.012  100.0
    Total                     1       0.012


Running xFoil......
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL
.

Running xFoil......
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL
.

Running xFoil......
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL
.

Running xFoil......
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL
.

Running xFoil......
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL


Running xFoil......
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL
. EGADS Info: 0 Objects, 0 Reference in Use (of 67) at Close!

----------------------------------------------------------------------
Ran 67 tests in 75.943s

OK (skipped=12)
 Cleaning up egadsInstance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 Cleaning up egadsInstance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 2185) at Close!
 Cleaning up egadsInstance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 2185) at Close!
 Cleaning up egadsInstance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 2185) at Close!
 Cleaning up egadsInstance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 2143) at Close!
 Cleaning up aflr4Instance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 0) at Close!
 Cleaning up aflr4Instance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 2189) at Close!
 Cleaning up aflr4Instance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 2185) at Close!
 Cleaning up aflr4Instance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 2189) at Close!
 Cleaning up aflr4Instance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 2659) at Close!
 Cleaning up aflr2Instance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 1050) at Close!
 Cleaning up aflr2Instance - 0
 EGADS Info: 0 Objects, 0 Reference in Use (of 1050) at Close!

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>set err4=0 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>REM Check CAPS training examples 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>if unit == training2018 mkdir C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\test\training2018   || exit /b 666 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>if unit == training2018 cd C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\test\training2018   || exit /b 666 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>if unit == training2018 xcopy C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\training\2018\data\* /Q /Y   || exit /b 666 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>if unit == training2018 C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\ESP\WIN64\test\template_avl   || set err4=1 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>if unit == training2018 bash.exe -x -e -c "for i in `ls wing*.csm | sort -f`; do time python runAll.py $i; done"   || set err4=1 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>REM Don't run examples because matplotlib actually plots, but nobody is there to close the window 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>REM if unit==training2018 bash.exe -x -e -c "for i in `ls exercise*.py | sort -f`; do time python $i; done" || set err4=1 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>set err1=0 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>set err2=0 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>set err3=0 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>if CAPS == OpenCSM (if NOT unit == pyOCSM (
set /p err1= 0<err1_tmp.out  
 set /p err2= 0<err2_tmp.out  
 if "" == "" (set /p err3=  0<err3_tmp.out )  else (set err3=0  ) 
) ) 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>echo off 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>set /a "err=0+0+0+0" 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\unitTest\pyCAPS>exit /b 0 

C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017\CAPS\aim\skeleton>exit 0 
[GNU C Compiler (gcc)] Sleeping for 5 seconds due to JENKINS-32191...
[GNU C Compiler (gcc)] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017')
[GNU C Compiler (gcc)] Successfully parsed console log
[GNU C Compiler (gcc)] -> found 0 issues (skipped 0 duplicates)
[GNU C Compiler (gcc)] Skipping post processing
[GNU C Compiler (gcc)] No filter has been set, publishing all 0 issues
[GNU C Compiler (gcc)] Repository miner is not configured, skipping mining
[Clang (LLVM based)] Sleeping for 5 seconds due to JENKINS-32191...
[Clang (LLVM based)] Parsing console log (workspace: 'C:\Users\jenkins\workspace\ESP_QuickTestCaps\7.4\CAPS\unit\WIN64.2017')
[Clang (LLVM based)] Successfully parsed console log
[Clang (LLVM based)] -> found 0 issues (skipped 0 duplicates)
[Clang (LLVM based)] Skipping post processing
[Clang (LLVM based)] No filter has been set, publishing all 0 issues
[Clang (LLVM based)] Repository miner is not configured, skipping mining
[Static Analysis] Reference build recorder is not configured
[Static Analysis] Obtaining reference build from same job (7.4,WIN64.2017,windows10x64)
[Static Analysis] Using reference build 'ESP_QuickTestCaps/CASREV=7.4,ESP_ARCH=WIN64.2017,buildnode=windows10x64 #25' to compute new, fixed, and outstanding issues
[Static Analysis] Issues delta (vs. reference build): outstanding: 0, new: 0, fixed: 0
[Static Analysis] Evaluating quality gates
[Static Analysis] -> PASSED - Total (any severity): 0 - Quality QualityGate: 1
[Static Analysis] -> All quality gates have been passed
[Static Analysis] Health report is disabled - skipping
[Static Analysis] Created analysis result for 0 issues (found 0 new issues, fixed 0 issues)
[Static Analysis] Attaching ResultAction with ID 'analysis' to build 'ESP_QuickTestCaps/CASREV=7.4,ESP_ARCH=WIN64.2017,buildnode=windows10x64 #26'.
[Checks API] No suitable checks publisher found.
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] done
Finished: SUCCESS