#Copyright (C) 2011 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_T651 Aluminum Wrought, Room Temp., Data from reference:
# R.F.Brodrick, G.A.Spiering, "Low Cycle Fatigue of Aluminum Alloys",
# ASTM J.of Matls, V7 N4 Dec 1972, pp.515-526
# Raw Material: 1.25 inch thick plate, Round 0.500 in. diam.
# 2.inch Radius Diametral specimens.
# No test mean stresses reported. Only one modulus reported.
#
#FileType= strain_life
#DataType= raw
#TIMEcol= 0
#NAME= AA6061_T651
#Name= Aluminum
#Stress_units= ksi
#Strain_units= strain
#Su=       43.2  ksi
#Sy=       40.1  ksi  0.2% offset
#E=       10100.
#%RA=   45.4  percent
#%Elong= 18.3 percent over 2 inch.
#TrueFractureStress= 69.2  ksi
#TrueFractureStrain= 0.61
#MonotonicStrengthCoefficient= 63.8
#MonotonicStrainHardeningExponent= 0.124
#BHN=   0.
#NO. FAT. PTS.=  12
#Tot Strain    2Nf  Stress  Mean   PlasStrain   Initial   NeuberRg
#_ Amp               Amp   Stress      Amp    Elas_Mod.
   .0254      152   50.4       0  .0204        10100.     227.4
   .0245      142  50.95       0  .0199        10100.     226.6
   .0241      198  50.15       0  .01915       10100.     222.0
   .0191      334  48.75       0  .01425       10100.     194. 
   .01825     300  48.65       0  .01345       10100.     189.4
   .0145      564  48.15       0  .00975       10100.     167.9
   .0130      898  45.7        0  .0085        10100.     154.9
   .0118      906  45.65       0  .0073        10100.     147.5
   .00565    8358  40.5        0  .00165       10100.      96.1
   .00510    7600  40.65       0  .0011        10100.      91.5
   .00395   15816  37.7        0  .00025       10100.      77.6
   .0038    16200  37.1        0  .00015       10100.      75.5
#
#