#The file is derived from ENDO, MORROW, J.OF MATLS., V4, 69 Table 6 page 168. #The derivations and additions have been made by the #members of the FD+E committee. 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 #MERCHANTABILITY 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= 113 # TI-8AL-1MO-1V ANNEALED HARDNESS ASSUMED ABOUT 40 RC # FROM 0.675in ROD Duplex annealed Q & T TO SU=148KSI # BHN 400 APPROX # Supplier: Reactive Metals, Niles Ohio Heat No. 291976 # #Webpage= https://fde.uwaterloo.ca/Fde/Materials/Titan/Ti8al1mo1v/ti8al1mov.html #FileType= strain_life #DataType= raw #TIMEcol= 0 #NAME= Titanium #NAME= TI8AL1MO1V #Stress_units= ksi #Strain_units= strain #Su= 147.9 #Sy= 145.9 #E= 17000. #%RA= 48. #BHN= 400. #FDUCTILITY= 0.66 #FSTRENGTH= 215 #ksi #StrainHardeningExponent= 0.078 #NO. FAT. PTS.= 5 #Tot Strain 2Nf Stress Mean Plastic Strain Initial #_ Amp Amp Stress Amp Elastic Mod. 0.077000 74. 172.88 0. 0.066000 16984. 0.045000 148. 162.88 0. 0.035500 16984. 0.021500 766. 148.37 0. 0.012500 16984. 0.012000 3040. 118.93 0. 0.005000 16984. 0.008000 8720. 111.39 0. 0.002000 16984. # #