See below also for ADVANCED ALGEBRAIC OPERATION INPUT: All data bases can be used without separate modification.

$ MAT.DATA FILE
$ MATERIAL PROPERTY FILE IN BRITISH SYSTEM
$ I D E G ALPHA RHO FYFU
$ NAME KIP/In**2 KIP/In**2 In/In/Deg_F KIP/In**3 K/In**2 K/In**2
STEL 29000. 11200. 0.0000065 0.000283565 36.0 60.0
MAT2 29000. 11200. 0.0000065 0.000000000
STELWT9X38 29000. 11200. 0.0000065 0.000283565
STELPIPE2 29000. 11200. 0.0000065 0.000000000
STELPIPE6 29000. 11200. 0.0000065 0.000283565
ALUMGIRDER 10000. 3850. 0.0000128 0.000095486
CNC8COLUMN 3620. 1360. 0.0000055 0.000086806
$ FOR PLOT: NO NON-LINEAR ALLOW BELOW; FOR USP: O K
NLINmateri 10000. 3750. 0.0000128 0.0000
NONLcontin 0.002 20. 0.0044 24. 0.010 26.77 $ (Epsilon Sigma)Pair
NONLcontin 0.020 30.65 $ (Epsilon Sigma)Pair
$ MATERIAL NON-LINEARITY PROPERTY NEXT ABOVE
$ FOR PLOT: NO NON-LINEAR ALLOW ABOVE; FOR USP: O K
END DATA
END DATA
$ MAT.DATA FILE
$ MATERIAL PROPERTY FILE IN METRIC SYSTEM
$ I D E G ALPHA RHO FYFU
$ NAME T/Cm**2 T/Cm**2 Cm/Cm/Deg_C T/Cm**3 T/Cm**2 T/Cm**2
STEL 2040. 785. 0.0000117 .00000784905 2.532 4.221
MAT2 2040. 785. 0.0000117 0.000000000
STELWT9X38 2040. 785. 0.0000117 0.00000784905
STELPIPE2 2040. 785. 0.0000117 0.000000000
STELPIPE6 2040. 785. 0.0000117 0.00000784905
ALUMGIRDER 705. 265. 0.0000230 0.00000264305
CNC8COLUMN 255. 106. 0.0000100 0.00000240278
$ FOR PLOT: NO NON-LINEAR ALLOW BELOW; FOR USP: O K
NLINmateri 705. 265. 0.0000230 0.0000
NONLcontin 0.002 1.410.0044 1.6920.010 1.887 $ (Epsilon Sigma)Pair
NONLcontin 0.020 2.161 $ (Epsilon Sigma)Pair
$ MATERIAL NON-LINEARITY PROPERTY NEXT ABOVE
$ FOR PLOT: NO NON-LINEAR ALLOW ABOVE; FOR USP: O K
END DATA
END DATA

ADVANCED ALGEBRAIC OPERATION INPUT DATA USAGE
SYSTEM INTERNATIONAL COMPUTATION WITH MAT.DAT IN BRITISH SYSTEM

$ MAT.DATA FILE
$ S I COMPUTATION USING MATERIAL PROPERTY FILE IN BRITISH SYSTEM
$ I D E G ALPHA RHO FYFU
$ NAME K/In**2 K/In**2 In/In/Deg_F K/In**3 K/In**2 K/In**2
$ NAME KN/mm**2 KN/mm**2 mm/mm/Deg_C KN/mm**3 KN/mm**2 KN/mm**2
MUL 4 K=4.44822 I=25.4
MUL OFF
MUL 4 0 K/I**2 K/I**2 1.8 K/I**3K/I**2K/I**2
STEL 29000. 11200. 0.0000065 0.000283565 36.0 60.0
MAT2 29000. 11200. 0.0000065 0.000000000
STELWT9X38 29000. 11200. 0.0000065 0.000283565
STELPIPE2 29000. 11200. 0.0000065 0.000000000
STELPIPE6 29000. 11200. 0.0000065 0.000283565
ALUMGIRDER 10000. 3850. 0.0000128 0.000095486
CNC8COLUMN 3620. 1360. 0.0000055 0.000086806
$ FOR PLOT: NO NON-LINEAR ALLOW BELOW; FOR USP: O K
NLINmateri 10000. 3750. 0.0000128 0.0000
MUL OFF
MUL 4 0 0 K/I**2 0 K/I**20 K/I**2
NONLcontin 0.002 20. 0.0044 24. 0.010 26.77 $ (Epsilon Sigma)Pair
NONLcontin 0.020 30.65 $ (Epsilon Sigma)Pair
MUL OFF
$ MATERIAL NON-LINEARITY PROPERTY NEXT ABOVE
$ FOR PLOT: NO NON-LINEAR ALLOW ABOVE; FOR USP: O K
END DATA
END DATA

ADVANCED ALGEBRAIC OPERATION INPUT DATA USAGE
METRIC COMPUTATION WITH MAT.DAT IN BRITISH SYSTEM

$ MAT.DATA FILE
$ METRIC COMPUTATION USING MATERIAL PROPERTY FILE IN BRITISH SYSTEM
$ I D E G ALPHA RHO FYFU
$ NAME K/In**2 K/In**2 In/In/Deg_F K/In**3 K/In**2 K/In**2
$ NAME T/Cm**2 T/Cm**2 Cm/Cm/Deg_C T/Cm**3 T/Cm**2 T/Cm**2
MUL 4 K=0.454 I=2.54
MUL OFF
MUL 4 0 K/I**2 K/I**2 1.8 K/I**3K/I**2K/I**2
STEL 29000. 11200. 0.0000065 0.000283565 36.0 60.0
MAT2 29000. 11200. 0.0000065 0.000000000
STELWT9X38 29000. 11200. 0.0000065 0.000283565
STELPIPE2 29000. 11200. 0.0000065 0.000000000
STELPIPE6 29000. 11200. 0.0000065 0.000283565
ALUMGIRDER 10000. 3850. 0.0000128 0.000095486
CNC8COLUMN 3620. 1360. 0.0000055 0.000086806
$ FOR PLOT: NO NON-LINEAR ALLOW BELOW; FOR USP: O K
NLINmateri 10000. 3750. 0.0000128 0.0000
MUL OFF
MUL 4 0 0 K/I**2 0 K/I**20 K/I**2
NONLcontin 0.002 20.0 0.0044 24.0 0.010 26.77 $ (Epsilon Sigma)Pair
NONLcontin 0.020 30.65 $ (Epsilon Sigma)Pair
MUL OFF
$ MATERIAL NON-LINEARITY PROPERTY NEXT ABOVE
$ FOR PLOT: NO NON-LINEAR ALLOW ABOVE; FOR USP: O K
END DATA
END DATA

ADVANCED ALGEBRAIC OPERATION INPUT DATA USAGE
SYSTEM INTERNATIONAL COMPUTATION WITH MAT.DAT
IN MIXED (S I & BRITISH) SYSTEM

$ MAT.DATA FILE
$ S I COMPUTATION USING MATERIAL PROPERTY FILE IN MIXED SYSTEM
$ I D E G ALPHA RHO FYFU
$ NAME KIP/In**2 KIP/In**2 In/In/Deg_F KIP/In**3 K/In**2 K/In**2
$ NAME KN/mm**2 KN/mm**2 mm/mm/Deg_C KN/mm**3 KN/mm**2 KN/mm**2
MUL 4 K=4.44822 I=25.4
MUL OFF
MUL 4 0 K/I**2 K/I**2 1.8 K/I**3K/I**2K/I**2
STEL 29000. 11200. 0.0000065 0.000283565 36.0 60.0
MAT2 29000. 11200. 0.0000065 0.000000000
STELWT9X38 29000. 11200. 0.0000065 0.000283565
STELPIPE2 29000. 11200. 0.0000065 0.000000000
STELPIPE6 29000. 11200. 0.0000065 0.000283565
ALUMGIRDER 10000. 3850. 0.0000128 0.000095486
CNC8COLUMN 3620. 1360. 0.0000055 0.000086806
$ FOR PLOT: NO NON-LINEAR ALLOW BELOW; FOR USP: O K
MUL OFF
       NLINmateri 68.9 26.5 0.0000230 0.0000
NONLcontin 0.002 .13790.0044 .16550.010 .1846 $ (Epsilon Sigma)Pair
NONLcontin 0.020 .2113 $ (Epsilon Sigma)Pair
$ MATERIAL NON-LINEARITY PROPERTY NEXT ABOVE
$ FOR PLOT: NO NON-LINEAR ALLOW ABOVE; FOR USP: O K
END DATA
END DATA

SECT.DAT can be made in this fashion in a bigger scale too.

Structure - Programming - Vibration - Foundation - Civil

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This page was last updated on September/9/1999 and Oct./10/2003 .