#Copyright (C) 2001 Fatigue Design + Evaluation Comm. of 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= 108 # AA 2024-T4 ALUM., wrought, Specimens from 3/4inch rod stock. # ENDO T. J. MORROW, J. OF MATERIALS, VOL.4, P.159,1969 # BHN ASSUMED 120, Strain Controlled Diametral testing # Converted to longitudinal. correction Jan.31, CCChu # NOTE: Data points are averages of several points # #FileType= strain_life #DataType= raw #TIMEcol= 0 #NAME= A2024C02 #NAME= AA2024-T4 #Name= Aluminum #Stress_units= ksi #Strain_units= strain #Su= 69.00 #Sy= 44.00 #E= 10196. #%RA= 35.0 #BHN= 120. #NO. FAT. PTS.= 8 #Tot Strain 2Nf Stress Mean Plastic Strain Initial #_ Amp Amp Stress Amp Elastic Mod. 0.072500 10. 88.50 0. 0.064000 10196. 0.044500 28. 86.00 0. 0.036000 10196. 0.029000 90. 80.93 0. 0.021500 10196. 0.018250 284. 76.00 0. 0.010900 10196. 0.012250 620. 68.00 0. 0.005200 10196. 0.008200 2000. 64.50 0. 0.001950 10196. 0.005600 8400. 57.00 0. 0.000150 10196. 0.004650 24800. 49.00 0. 0.000000 10196. # #