#Copyright (C) 2001 B.N. Leis #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 # # Fitted Data Only! # 2024-T351 AL, B.N. Leis UoWaterloo, # 4.2Cu 1.2Mg 0.5Mn 0.3Si 0.2ZN 0.1Fe TRACE_Cr, Al REST. # BHN not known. Info taken from Leis MSc Thesis fig 17 #Fn= 267 # #FileType= strain_life #DataType= fitted #TIMEcol= 0 #NAME= AA-2024-T351 #NAME= LEIS2024 #Name= Aluminum #Stress_units= ksi #Strain_units= strain #Su= 70.00 #Sy= 52.00 #E= 10100. #%RA= 0.0 #BHN= 0. #NO. FAT. PTS.= 9 # AA-2024-T3 LEIS2024 BHN= 0 Fn= 0 #_ Monotonic Props. Cyclic Props. #ELAS. MOD.= 10100. KSI, 70. GPA K' = 127.8 KSI, 881.MPA #YIELD,0.2%= 52. KSI, 359. MPA N' = 0.1314 #ULT. STRG.= 70. KSI, 483. MPA F. STRG COEF= 115.0 KSI, 793.MPA #K = 0.0 KSI, 0. MPA F.STRG EXP, b=-0.0897 #N = 0.0000 FAT DUCT COEF= 0.4501 #RED. IN AREA = 0.0 F.DUCT EXP, c=-0.6826 #T. FRAC. STG.= 0.0 KSI, 0. MPA Exp Cyc Yld = 56. Ksi, 389.MPA #T. FRAC. STR.= 0.000 Fit Cyc Yld = 58. Ksi, 402.MPA #No. fatigue data points= 9 # # NOTE!! The Following Points are <b>FITTED DATA:</b> #UNITS= KSI #Stress_Units= KSI #_Total Strain 2Nf Stress Mean Plastic Strain Initial #_ Amp Amp Stress Amp Elastic Mod. 0.46151 1 115.0 0. 0.45012 10100. #Fitted_point 0.29114 2 108.1 0. 0.28044 10100. #Fitted_point 0.15989 5 99.6 0. 0.15003 10100. #Fitted_point 0.10274 10 93.6 0. 0.09347 10100. #Fitted_point 0.06694 20 87.9 0. 0.05824 10100. #Fitted_point 0.03917 50 81.0 0. 0.03116 10100. #Fitted_point 0.02695 100 76.1 0. 0.01941 10100. #Fitted_point 0.01917 200 71.5 0. 0.01209 10100. #Fitted_point 0.01299 500 65.9 0. 0.00647 10100. #Fitted_point 0.01016 1000 61.9 0. 0.00403 10100. #Fitted_point 0.00827 2000 58.2 0. 0.00251 10100. #Fitted_point 0.00665 5000 53.6 0. 0.00134 10100. #Fitted_point 0.00582 10000 50.3 0. 0.00084 10100. #Fitted_point 0.00521 20000 47.3 0. 0.00052 10100. #Fitted_point 0.00459 50000 43.6 0. 0.00028 10100. #Fitted_point 0.00423 100000 40.9 0. 0.00017 10100. #Fitted_point 0.00392 200000 38.5 0. 0.00011 10100. #Fitted_point 0.00357 500000 35.4 0. 0.00006 10100. #Fitted_point 0.00333 1000000 33.3 0. 0.00004 10100. #Fitted_point 0.00312 2000000 31.3 0. 0.00002 10100. #Fitted_point 0.00287 5000000 28.8 0. 0.00001 10100. #Fitted_point 0.00269 10000000 27.1 0. 0.00001 10100. #Fitted_point 0.00253 20000000 25.5 0. 0.00000 10100. #Fitted_point 0.00232 50000000 23.4 0. 0.00000 10100. #Fitted_point 0.00218 100000000 22.0 0. 0.00000 10100. #Fitted_point 0.00205 200000000 20.7 0. 0.00000 10100. #Fitted_point 0.00189 500000000 19.1 0. 0.00000 10100. #Fitted_point 0.00177 1000000000 17.9 0. 0.00000 10100. #Fitted_point #Here is the bottom part of the html graph/calc wrapper----------- # #