#Copyright (C) 2011 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 # # AA5052-H32 Aluminum from 4.8mm sheet, Kaiser Aluminum # (may be in transvese direction) # Material cyclically hardens substantially (31% at 0.01 strain Ampl.) # Ref.: W.A.Wong, "Monotonic and Cyclic Fatigue Properties of Automotive # Aluminum Alloys, SAE paper 840120 # Data digitized from graphs and may contain errors. # #FileType= strain_life #DataType= raw #TIMEcol= 0 #NAME= AA5052-H32 #NAME= Aluminum #Stress_units= mpa #Strain_units= strain #Sy= 167. mpa 0.2pc offset #Su= 231. #eu= 0 #strain at Su not reported #E= 69600. #FractureStrain= 0.95 #FractureStress= 473. #monotonic_K= 371 #monotonic_n= 0.156 #BHN= 0. not reported #%RA= 61.5 % #StrAmpl 2Nf StsAmpl So PlasStrAmpl IniMod NeuberStressAmpl 0.01470 159 237 0 0.01130 69600 493 0.01428 249 242 0 0.01080 69600 491 0.01161 369 232 0 0.00828 69600 433 0.00991 561 230 0 0.00660 69600 399 0.00882 652 227 0 0.00556 69600 373 0.00837 777 221 0 0.00520 69600 359 0.00692 1166 225 0 0.00369 69600 330 0.00696 1289 225 0 0.00373 69600 330 0.00594 2551 217 0 0.00281 69600 300 0.00499 4828 216 0 0.00189 69600 274 0.00439 6157 212 0 0.00134 69600 255 0.00411 8056 214 0 0.00103 69600 247 0.00393 11952 210 0 0.00091 69600 240 0.00351 12937 208 0 0.00053 69600 225 0.00281 18238 181 0 0.00020 69600 188 0.00335 28663 205 0 0.00040 69600 219 0.00259 31658 173 0 0.00010 69600 177 0.00218 122551 151 0 0.00000 69600 151 0.00211 194867 147 0 0.00000 69600 147 0.00192 1908390 134 0 0.00000 69600 134 0.00184 2274110 128 0 0.00000 69600 128 # #