#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 6061_T6 Aluminum Wrought, Data from reference: # Chung, Y.S. and A.Abel, ASTM STP 942 1988. # 0.15wt%Cu 1.45Mg .04Mn .59Si .03Zn from rod stock # 12mm gauge length # #FileType= strain_life #DataType= raw #TIMEcol= 0 #NAME= AA6061_T6 #Name= Aluminum #Stress_units= ksi #Strain_units= strain #Su= 0. #Sy= 37.4 #E= 10100. #%RA= 0 #BHN= 0. #NO. FAT. PTS.= 13 #Tot Strain 2Nf Stress Mean Pl Str Initial NeuberRg #_ Amp Amp Stress Amp Elas Mod. .0156 192 43.2 0. .01132 10100 165. .0119 342 41.9 0. .00775 10100 141.9 .00945 700 40.9 0. .0054 10100 125. .00780 1172 40.3 0. .0038 10100 112.7 .00725 1384 39.1 0. .00338 10100 107. .00555 2420 37.2 0. .0018 10100 91.3 .00555 2980 37.9 0. .0018 10100 92.2 .00455 4420 35.1 0. .0011 10100 80.3 .00455 5980 35.6 0. .0010 10100 80.9 .00415 7640 33.8 0. .0008 10100 75.3 .00380 11800 33.0 0. .00053 10100 71.2 .00325 23260 30.6 0. .00022 10100 63.4 .00315 41760 30.3 0. .00015 10100 62.1 # #