#
#Copyright (C) 2015 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 # CSA G40.21-350W, or ASTM-A572 Grade 50, 9.5mm plate # Specimen polished, smooth square 12.5 x 9.5mm, # Nominal Chem.: 0.23C 0.50-1.50Mn .04P .05S .35Si # Ref. K.Ghahremani, MSc thesis U.ofWaterloo, 2010. # HRB= 89 before sim. # Elongation= 31% over 10mm. # NOTE!: For BS7910 FADs required Tags are: # #FileType= #DataType= #Sy= #Su= #E= # #Stress_units= #Strain_units= # #FileType= strain_stress #DataType= engineering #Can be "engineering" or "true" #NAME= ASTM-A572gr50 #NAME= CSA-G40.21-350W #NAME= Steel #Stress_units= mpa #Strain_units= strain #Sy= 388. mpa #Su= 571. mpa #eu= 0.156 #strain at Su #E= 201600. mpa # MSc thesis #FractureStrain= 0.70 PhD thesis #FractureStress= 676 mpa (not reported. Used K'=676 PhD thesis ) #monotonic_K= 494 mpa PhD thesis #monotonic_n= 0.036 PhD thesis #BHN= 200. from PhD thesis #%RA= 49. % PhD thesis #file can be found at: #http://fde.uwaterloo.ca/Fde/Materials/Steel/Other/Astm-A572/steel350W_tenSS.txt 0 0 0.00069 136.5 0.00112 225.9 0.00167 335.4 0.00196 393.912 0.00205 398.628 0.00213 397.299 0.00221 397.982 0.00233 394.645 0.00244 393.32 0.00251 392.661 0.00263 389.322 0.00281 389.353 0.00303 388.718 0.00327 392.116 0.00331 390.108 0.00362 388.816 0.00392 389.539 #0.0018637 398.845 #0.00367812 390.873 0.00458977 392.001 0.00641207 393.119 0.00853103 386.281 0.0091411 389.684 0.0121796 393.063 0.0149135 395.309 0.0176623 414.601 0.019799 428.216 0.0252797 447.481 0.0307604 466.746 0.0362391 483.738 0.0444518 502.976 0.0517499 517.678 0.0596532 530.101 0.0699848 542.5 0.0827429 552.603 0.092158 558.193 0.105518 562.609 0.120397 568.145 0.138005 570.247 0.155916 571.209 #Ultimate strain, stress #Rest are engineering str,sts, commented out: #0.17777 568.723 #0.188698 568.617 #0.19932 566.24 #0.219045 559.23 #0.234214 548.855 #0.248167 536.219 #0.26363 515.614 #0.277271 493.89 #0.288787 471.051 #0.299691 443.672 #0.306352 424.289 # #