#
#All of the data below was derived, but not copied, from the NASA Tech. #Note D-1574.The derivations and additions have been made by the members #of the FD+E committee of the SAE. Thus: # #Copyright (C) 1999 Fatigue Design + Evaluation Committee of the SAE. #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 # #Fn= 106 # ALUMINUM, 1100 WROUGHT, LONGITUDINAL, Diametral Hourglass Specimens # cut from as-received bar stock, Strains converted to Longitudinal direction. # Nominal Composition: Si+Fe=1.0% .20Cu max, .05Mn max, .10Zn, Al remainder # SMITH ET AL, NASA TN D-1574,1963 # BHN 26.01 #Webpage= https://fde.uwaterloo.ca/Fde/Materials/Alum/AA1100/aa1100_non_os.html # #FileType= strain_life #DataType= raw #TIMEcol= 0 #NAME= AA1100 #Name= Aluminum #Stress_units= ksi #Strain_units= strain #Su= 17. #Sy= 14.01 #E= 10000. #%RA= 87.5 #BHN= 26.01 #NO. FAT. PTS.= 12 #Tot Strain 2Nf Stress Mean Plastic Strain Initial #_ Amp Amp Stress Amp Elastic Mod. 0.200700 22. 21.03 0. 0.198600 9993. 0.120600 54. 17.98 0. 0.118800 9993. 0.060500 146. 14.94 0. 0.059000 9993. 0.030400 564. 12.04 0. 0.029200 9993. 0.014400 1568. 11.02 0. 0.013300 9993. 0.006300 4240. 8.99 0. 0.005400 9993. 0.003300 12640. 8.99 0. 0.002400 9993. 0.002300 25600. 8.56 0. 0.001500 9993. 0.001300 208000. 7.54 0. 0.000500 9993. 0.001100 410000. 7.54 0. 0.000300 9993. 0.000900 834000. 7.54 0. 0.000200 9993. 0.000700 2000000. 6.96 0. 0.000100 9993. #Runout #Here is the bottom part of the html graph/calc wrapper----------- # #