Nonlinear Compression Only gti file

*TITLE 'EXNL01 - HIGHLY NONLINEAR COMPRESSION-ONLY TEST'
STRUDL 'EXNL01' 'HIGHLY NONLINEAR COMPRESSION-ONLY TEST'
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$* ** PROBLEM DESCRIPTION: Sample problem for Nonlinear Analysis.
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PRINT GEN OFF
UNITS FEET POUNDS DEGREES
GEN 2 JOI ID 1 100 X -8.916,-1 Y -14.5
MOD 19 ID 1 Y 0.97
JOINT COORD
1001 -2.83 4.907
1002 2.83 4.907
GEN 2 JOINTS CYL Z ID 21 100 R 6.083 1 TH 180 LZ 0 OFFSET 1001
MOD 6 ID 1 TH -10
GEN 2 JOI CYL Z ID 28 100 R 11.75 1 TH 115 LZ 0
MOD 11 ID 1 TH -5
GEN 2 JOI CYL Z ID 40 100 R 6.083 1 TH 50 LZ 0 OFFSET 1002
MOD 5 ID 1 TH -10
GEN 2 JOI ID 46 100 X 8.916 1 Y 3.937
MOD 19 ID 1 Y -0.97
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TYPE PLANE FRAME
GEN 64 MEMBS ID 1 1 FROM 1 1 TO 2 1
TYPE PLANE TRUSS
GEN 63 MEMBS ID 101 1 FROM 102 1 TO 2 1
STATUS SUPPORT JOI 1 65 102 TO 164
JOINT RELEASES
1 65 MOM Z
DELETIONS
JOINTS 101 165
ADDITIONS
INACTIVE JOINTS 1001 1002
UNITS INCHES
PRINT JOINT COORDINATES
UNITS INCHES
CONSTANTS
E 3.6E6 MEMBERS 1 TO 64
E 1.E6 MEMBERS 101 TO 163
MEMBER DIMENSIONS
1 TO 64 RECT B 12 H 10
MEMBER PROP PRIS
101 TO 120 144 TO 163 AX 139.68
121 TO 143 AX 152.88
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PLOT PROJECTION
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LOADING 1 'UNIFORM LOAD OF 1 KIP/FT'
MEMBER LOADS
21 TO 44 FORCE Y GLO UNIW -83.33
LOADING 2 'TEXT LOAD TO MATCH ANSYS RESULTS'
JOINT LOADS
21 TO 45 FORCE Y -713.2 $ = 17830 LBS
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LOAD LIST 2
NONLINEAR EFFECTS
COMPRESSION ONLY MEMBERS 101 TO 163
MAXIMUM NUMBER OF CYCLES 1
CONVERGENCE TOLERANCE EQUIL 0.00001
NONLINEAR ANALYSIS REDUCE BAND
LIST LOADS DISPL
NONLINEAR ANALYSIS CONT
LIST LOADS DISPL
NONLINEAR ANALYSIS CONTINUE
MAXIMUM NUMBER OF CYCLES 20
NONLINEAR ANALYSIS CONTINUE
OUTPUT DECIMAL 4
OUTPUT ORDERED
LIST DISPLACEMENTS
LIST LOADS
LIST REACTIONS
LIST FORCES
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CONVERGENCE TOLERANCE DISPL 0.00001
MAXIMUM NUMBER OF CYCLES 25
NONLINEAR ANALYSIS
LIST DISPLACEMENTS
LIST LOADS
LIST REACTIONS
LIST FORCES
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FINISH