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#Copyright (C) 2013 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 # A36 Steel Hot Rolled # Machined from 5/8 inch hot rolled plate. # Ref.: R.J.Mattos, F.V.Lawrence, "Estimation of the Fatigue Crack Initiation # Life in Welds Using Low Cycle Fatigue Concepts," Fracture Control Rep.19 # Univ. of Illinois, Oct. 1975. # 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-A36 #NAME= HotRolled #NAME= Steel #Stress_units= mpa #Strain_units= strain #Sy= 224. mpa = 32.5 ksi #Su= 414. mpa = 60.0 ksi #eu= 0.14 #strain at Su #E= 190000 mpa 27500 ksi #FractureStrain= 1.19 #FractureStress= 952 mpa = 138 ksi #monotonic_K= 780 mpa, 113 ksi #monotonic_n= 0.258 #BHN= 0. not reported #%RA= 69.7 % #From initial MattosStress-Strain plot 0 0 0.00036 72 0.00073 143 0.00146 224 0.00206 220 0.00274 224 # 0.00371 229 # 0.00474 230 # 0.00647 229 # 0.00750 230 # 0.00956 230 # 0.01121 232 # 0.01253 238 # 0.01367 243 # 0.01470 252 # 0.01608 264 #From Mattos Stress vs Plastic strain #(converted back to Engr.SS) #EngrStr EngrSts_mpa 0.00301 221 0.00398 224 0.00511 224 0.00698 224 0.00793 220 0.00891 221 0.00991 220 0.01193 228 0.01392 238 0.01610 250 0.02004 273 0.02371 285 0.02852 295 0.03146 301 0.03696 313 0.04237 326 0.05977 357 0.07941 371 0.09925 393 0.11768 395 0.13824 399 0.15728 397 0.17514 400 #Ultimate Stress # #