#All of the data below was derived, but not copied, from the #NASA Tech. Note D-7532, 1974 #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 #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= 166 # TI-5AL-2.5SN AS RECEIVED, VACUUM ANNEALED, LONGITUDINAL # NACHTIGALL, NASA TN D-7532, 1974 # MATERIALS DATA BOOK SPECS HARNESS AT 36 RC ? # #FileType= strain_life #DataType= raw #TIMEcol= 0 #NAME= TI-5AL-2.5SN_Titanium #Stress_units= ksi #Strain_units= strain #Su= 125. #Sy= 120. #E= 17300. #%RA= 0.0 #BHN= 0. #NO. FAT. PTS.= 11 #Tot Strain 2Nf Stress Mean Plastic Strain Initial #_ Amp Amp Stress Amp Elastic Mod. 0.053200 106. 132.56 0. 0.045550 17288. 0.032950 266. 121.69 0. 0.025950 17288. 0.023000 414. 118.93 0. 0.016150 17288. 0.016750 830. 114.43 0. 0.010150 17288. 0.010750 1936. 113.13 0. 0.004200 17288. 0.007250 4400. 100.51 0. 0.001450 17288. 0.007350 5200. 103.99 0. 0.001350 17288. 0.008100 5860. 101.96 0. 0.002200 17288. 0.006350 8820. 97.18 0. 0.000750 17288. 0.006450 10480. 99.35 0. 0.000700 17288. 0.005450 31080. 91.81 0. 0.000150 17288. # #