SAE Standard Fatigue Data File format

#SAE Standard Fatigue Data File format #
Pick one: #FDE_plot #FDE_fit # #

#Copyright (C) 2019  F.D.E. Committee
#This data file is free software - you can redistribute it and/or
#modify it under the terms of the GNU General Public License as
#published by the Free Software Foundation; either version 2 of the
#license, or (at your option) any later version.
#This data file is distributed in the hope that it will be useful,
#but WITHOUT ANY WARRANTY - without even the implied warranty of
#MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
#GNU General PUblic License for more details.
#You should have received a copy of the GNU General PUblic License
#along with this program - if not, write to the Free Software
#Foundation, Inc., 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA
#Try also their web site: http://www.gnu.org/copyleft/gpl.html
#
# HSLA-345XK (SAE950XK) USS-ExTen-F50 Sheet steel tests
# Program to test sheet to sheet variablility.
# Ref.: J.M.Holt, B.K.Stewart, "Train-Contolled Fatigue Properties of
# USS EX-TEN F50 Steel," SAE Paper 790460 Feb.26, 1979
# Tested by J.A. Nicholson.
# !
# Note! Change from paper:  
# Emod taken from long life tests and then compute Plastic Strain

#FileType= strain_life
#DataType= raw
#TIMEcol= 0
#NAME=  UssEX10F50
#NAME=  SAE950XK
#NAME=  HSLA-345-XK   
#UNITS= mpa
#Stress_units= mpa
#Below are average  Sy, Su  etc.
#Su= 377 mpa  54.7 ksi
#Sy= 455      66.0 ksi
#E=  204400.
#%RA= 67.3
#%Elongation= 33. % over 2 inch, 
#BHN=  0.
#FractureStress=  0.0
#FractureStrain=  0.0
#BHN= 0  not reported.

#StrAmpl 2Nf StsAmpl So PlsStrAmpl Emod_mpa 
#Sheet-11       
#Heat 1, Coil No.6, Sheet 11. , Sy=55.2, Su=69.1, 69.7%RA                        
#.07C .38Mn .003P .006S .033Si .008N .029Cb  - Ce .085Al
 0.00838 2090 413 0 0.00634 202700 
 0.00835 2560 417 0 0.00629 202700 
 0.00504 6226 370 0 0.00321 202700 
 0.00502 4088 380 0 0.00315 202700 
 0.00502 6244 363 0 0.00323 202700 
 0.00254 30820 307 0 0.00103 202700 
 0.00151 368950 254 0 0.00026 202700 
 0.00148 539814 305 0 0.00000 202700 
 0.00102 2212588 200 0 0.00003 202700 #runout

#Sheet-05C
#Heat 1, Coil No.5, Sheet C. , Sy=53.7, Su=63.6 64.0%RA                          
#.06C .36Mn .004P .008S .013Si .007N .029Cb .012Ce .072Al
 0.00751 1850 390 0 0.00561 205100 
 0.00514 3252 364 0 0.00337 205100 
 0.00502 4000 361 0 0.00326 205100 
 0.00256 17620 305 0 0.00107 205100 
 0.00155 115572 260 0 0.00028 205100 
 0.00153 111240 257 0 0.00028 205100 
 0.00100 1716320 201 0 0.00002 205100 
 0.00098 2025600 196 0 0.00002 205100 #runout

#Sheet-05T       
#Heat 1, Coil No.5, Sheet T. , Sy=53.6, Su=64.0 68.2%RA                          
#.06C .36Mn .004P .008S .013Si .007N .029Cb .012Ce .072Al
 0.00752 1200 390 0 0.00565 208000 
 0.00751 2228 394 0 0.00562 208000 
 0.00520 3806 360 0 0.00347 208000 
 0.00506 2922 362 0 0.00332 208000 
 0.00254 30394 303 0 0.00108 208000 
 0.00154 175864 275 0 0.00022 208000 
 0.00152 254170 250 0 0.00032 208000 
 0.00124 706913 236 0 0.00011 208000 
 0.00104 1877020 212 0 0.00002 208000 
 0.00100 2208128 203 0 0.00002 208000 #runout
       
#Sheet-06F       
#Heat 1, Coil No.6, Sheet F. , Sy=552.6 Su=67.6 77.0%RA                          
#.06C .36Mn .003P .007S .014Si .008N .029Cb .014Ce .075Al
 0.01000 968 438 0 0.00780 198800 
 0.00970 459 441 0 0.00748 198800 
 0.00512 2930 376 0 0.00323 198800 
 0.00392 6880 342 0 0.00220 198800 
 0.00355 9683 371 0 0.00168 198800 
 0.00311 7000 324 0 0.00148 198800 
 0.00253 45800 282 0 0.00111 198800 
 0.00250 33270 282 0 0.00108 198800 
 0.00164 52962 291 0 0.00018 198800 
 0.00162 145992 280 0 0.00021 198800 
 0.00146 173124 273 0 0.00009 198800 
 0.00108 1009214 206 0 0.00004 198800 #runout
       
#Sheet-02
#Heat 2, Coil No.4, Sheet 2. , Sy=50.4, Su=62.2 69.0%RA                          
#.06C .38Mn .005P .013S .027Si .005N .021Cb .010Ce .037Al
 0.00866 1360 402 0 0.00664 199000 
 0.00500 4092 348 0 0.00325 199000 
 0.00499 2828 356 0 0.00320 199000 
 0.00256 9800 316 0 0.00097 199000 
 0.00252 13874 302 0 0.00100 199000 
 0.00148 154000 237 0 0.00029 199000 
 0.00148 122300 270 0 0.00012 199000 
 0.00127 2121940 224 0 0.00014 199000 #runout
 0.00126 880400 223 0 0.00014 199000 
       
#Sheet-03 0.133in thick
#Sheet 3. , Sy=61.2, Su=68.8, 60.1%RA
#.06C .38Mn .007P .017S .030Si .004N .022Cb .020Ce .050Al 190ppm_O
 0.00751 1190 400 0 0.00565 215000 
 0.00556 1730 391 0 0.00374 215000 
 0.00504 2960 363 0 0.00335 215000 
 0.00258 25020 308 0 0.00115 215000 
 0.00150 106340 254 0 0.00032 215000 
 0.00139 312014 270 0 0.00014 215000 
 0.00101 998160 227 0 0.00000 215000 
 0.00079 2588000 163 0 0.00003 215000 #runout
       
#Sheet-07
#Heat 3, Coil No.9, Sheet 7. , Sy=57.5, Su=66.6, 63.4%RA                         
#.07C .36Mn .006P .015S .017Si .006N .026Cb .015Ce .054Al
 0.00865 1542 380 0 0.00677 202000 
 0.00532 4400 350 0 0.00359 202000 
 0.00501 1840 347 0 0.00329 202000 
 0.00319 5780 336 0 0.00153 202000 
 0.00252 15748 292 0 0.00107 202000 
 0.00152 95058 272 0 0.00017 202000 
 0.00148 150540 256 0 0.00021 202000 
 0.00130 347300 246 0 0.00008 202000 
 0.00098 2292840 207 0 0.00000 202000 #runout
#
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