#Copyright (C) 2010 Fatigue Design + Evaluation Comm. #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 MERCHANTA- #BILITY 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 # # AA 6351_T6 Aluminum Wrought, Data from reference: # Chung, Y.S. and A.Abel, ASTM STP 942 1988. # 0.05wt%Cu 0.51Mg .15Mn .85Si .05Zn .03Fe # 12mm gauge length # #FileType= strain_life #DataType= raw #TIMEcol= 0 #NAME= AA6351_T6 #Name= Aluminum #Stress_units= ksi #Strain_units= strain #Su= 0. #Sy= 42.1 #E= 10160. #%RA= 0 #BHN= 0. #NO. FAT. PTS.= 13 #Tot Strain 2Nf Stress Mean Plastic Strain Initial #_ Amp Amp Stress Amp Elastic Mod. 0.01495 152 47.4 0.0 0.01028 10160. 0.01295 224 46.8 0.0 0.00835 10160. 0.01095 420 46.3 0.0 0.00639 10160. 0.00800 694 44.0 0.0 0.00367 10160. 0.00753 1006 43.2 0.0 0.00328 10160. 0.00650 1432 42.4 0.0 0.00233 10160. 0.00645 1892 42.8 0.0 0.00224 10160. 0.00520 3140 40.3 0.0 0.00124 10160. 0.00430 8400 38.6 0.0 0.00050 10160. 0.00380 15640 36.0 0.0 0.00026 10160. 0.00370 22400 35.5 0.0 0.00021 10160. 0.00335 46760 33.4 0.0 0.00006 10160. 0.00325 57560 32.6 0.0 0.00004 10160. # #