#Copyright (C) 2021 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 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 # # AA5456-H311 Wrought Aluminum BHN=95 # Bar stock as received # Chem.: 5.1Mg .75Mn .12Cr .25Sn .20Ti Max Values: .40Si .40Fe .10Cu # Ref.: R.W.Smith M.H.Hirschberg S.S.Manson, "Fatigue Behavior # Ref.: of Materials under Strain Cycling in Low and intermediate # Ref.: Life Range," NASA Tech. Note D-1574, April 1963 # #FileType= strain_life #DataType= raw #TIMEcol= 0 #NAME= AA5456-H311 #NAME= WroughtAlum #Stress_units= ksi #Strain_units= strain #Sy= 34.0 ksi #Su= 58.0 #E= 10000. #%RA= 34.6 % #BHN= 95. #FractureStress= 82. ksi #FractureStrain= 0.42 # #StrAmpl 2Nf StsAmp So PlasStrAmpl Emod 0.032200 108. 63.53 0. 0.025800 10000. 0.016000 350. 59.03 0. 0.010100 10000. 0.009900 988. 55.40 0. 0.004400 10000. 0.006500 3840. 50.04 0. 0.001500 10000. 0.004400 11900. 43.95 0. 0.000000 10000. 0.003600 45600. 35.97 0. 0.000000 10000. 0.003300 130200. 32.49 0. 0.000000 10000. 0.003000 180600. 29.44 0. 0.000000 10000. 0.002600 260000. 25.96 0. 0.000000 10000. 0.002400 732000. 23.50 0. 0.000000 10000. 0.002200 1834000. 22.05 0. 0.000000 10000. # #