#saeinput FDE_fit SAE_Standard_File #
# # Copyright (C) 1999 Fatigue Design & Evaluation Comm. 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 # #--------------------------------------------------------------------------- # Source: The data file was derived from information in the paper: # R.I. Stephens, H.D.Berns, R.A.Chernenkoff, R.L.Indig, S.K.Koh, D.J.Lingenfelser # M.R.Mitchell, R.A.Testin, C.C.Wigant, "Low Cycle Fatigue of A356-T6 Cast Aluminum # Alloy - A Round-Robin Test Program, SAE SP-760, paper 881701, 1988. # AA-A356-T6 Cast Al, approx ISO:(Al Si7) # (the A implies more ductile than 356-T6) # SAE FD&E Round Robbin test results, all data of 3 batches # .01Cu .01Fe .01Mn 7.25Si .36Mg .01Zn .02Ti # Mod. reported as 10000ksi, changed to 10500(F.A.C.) # #FileType= strain_life #DataType= fitted #Ford= 519 #TIMEcol= 0 #NAME= Cast #NAME= A356-T6 #UNITS= KSI #Stress_units= ksi #Su= 38.00 #Sy= 32.50 #E= 10500. #%RA= 3.5 #BHN= 0. #NO. FAT. PTS.= 50 #Tot Strain 2Nf Stress Mean Plastic Strain Initial # Amp Amp Stress Amp Elastic Mod. # # Cast A356-T6 BHN= 0. Fn= 519 # Monotonic Props. Cyclic Props. #ELAS. MOD.= 10500. KSI, 72. GPA K' = 166.4 KSI, 1147.MPA #YIELD,0.2%= 32. KSI, 224. MPA N' = 0.2055 #ULT. STRG.= 38. KSI, 262. MPA F. STRG COEF= 81.1 KSI, 559.MPA #K = 0.0 KSI, 0. MPA F.STRG EXP, b=-0.1150 #N = 0.0000 FAT DUCT COEF= 0.0302 #RED. IN AREA = 3.5 F.DUCT EXP, c=-0.5595 #T. FRAC. STG.= 0.0 KSI, 0. MPA Exp Cyc Yld = 46. Ksi, 320.MPA #T. FRAC. STR.= 0.000 Fit Cyc Yld = 42. Ksi, 292.MPA #No. fatigue data points= 50 # # NOTE!!! The Following Points are FITTED DATA: #UNITS= KSI #Stress_Units= KSI # Total Strain 2Nf Stress Mean Plastic Strain Initial # Amp Amp Stress Amp Elastic Mod. 0.03792 1 81.1 0. 0.03019 10500. #Fitted_point 0.02762 2 74.9 0. 0.02049 10500. #Fitted_point 0.01869 5 67.4 0. 0.01227 10500. #Fitted_point 0.01425 10 62.2 0. 0.00833 10500. #Fitted_point 0.01112 20 57.5 0. 0.00565 10500. #Fitted_point 0.00831 50 51.7 0. 0.00338 10500. #Fitted_point 0.00684 100 47.8 0. 0.00230 10500. #Fitted_point 0.00576 200 44.1 0. 0.00156 10500. #Fitted_point 0.00471 500 39.7 0. 0.00093 10500. #Fitted_point 0.00412 1000 36.6 0. 0.00063 10500. #Fitted_point 0.00365 2000 33.8 0. 0.00043 10500. #Fitted_point 0.00316 5000 30.5 0. 0.00026 10500. #Fitted_point 0.00285 10000 28.1 0. 0.00017 10500. #Fitted_point 0.00259 20000 26.0 0. 0.00012 10500. #Fitted_point 0.00230 50000 23.4 0. 0.00007 10500. #Fitted_point 0.00210 100000 21.6 0. 0.00005 10500. #Fitted_point 0.00193 200000 19.9 0. 0.00003 10500. #Fitted_point 0.00173 500000 17.9 0. 0.00002 10500. #Fitted_point 0.00159 1000000 16.6 0. 0.00001 10500. #Fitted_point 0.00147 2000000 15.3 0. 0.00001 10500. #Fitted_point 0.00132 5000000 13.8 0. 0.00001 10500. #Fitted_point 0.00121 10000000 12.7 0. 0.00000 10500. #Fitted_point 0.00112 20000000 11.7 0. 0.00000 10500. #Fitted_point 0.00101 50000000 10.6 0. 0.00000 10500. #Fitted_point 0.00093 100000000 9.8 0. 0.00000 10500. #Fitted_point #