#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 5454-H34  Aluminum Wrought, Room Temp., Data from reference:
# Cold worked to "half-hard"
# 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. 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= AA544-H34
#NAME= half_hard
#Name= Aluminum
#Stress_units= ksi
#Strain_units= strain
#Su=       43.6  ksi
#Sy=       37.2  ksi  0.2% offset
#E=       10120.
#%RA=    23.8  percent
#%Elong= 11.3 percent over 2 inch.
#TrueFractureStress= 54.1  ksi
#TrueFractureStrain= 0.27
#MonotonicStrengthCoefficient= 59.0
#MonotonicStrainHardeningExponent= 0.856
#BHN=   0.
#NO. FAT. PTS.=  11
#Tot Strain   2Nf  Stress  Mean   PlasStrain  Initial  NeuberRg
#_ Amp               Amp   Stress      Amp    Elas_Mod.
0.004       21734     36.15     0     0.0004     10120     76.5
0.00405     21386     36.95     0     0.0004     10120     77.8
0.0046      12608     37.3      0     0.0009     10120     83.3
0.005        8492     38.65     0     0.00115    10120     88.4
0.00935      1460     42.6      0     0.00515    10120     127.0
0.00985      1100     43.9      0     0.0055     10120     132.3
0.0149        418     47.9      0     0.0103     10120     170.0
0.0152        422     45.55     0     0.0107     10120     167.4
0.0198        200     47.3      0     0.0151     10120     194.7
0.02075       150     47.7      0     0.01605    10120     200.2
0.02315       146     47.75     0     0.01845    10120     211.5
#
#