F.D.+E. Cyclic Stress-Strain Model from U.Waterloo Calc. Site

# #F.D.+E. Cyclic Stress-Strain Model from U.Waterloo Calc. Site # #

F.D.+E. pdStressStrain.f from UoWaterloo Calc. Site

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#

Your material file (its a Digital-Fitted Curve. Replace it with your own if you wish): #

#
#Copyright (C) 2015  F.D.E. Committee
#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
#
# Note!:  This is a fitted file/curve 
# Merged files of  GGG 60  ASTM 80.55.06  Nodular Iron
# Ref.: M. Hueck, W.Schuetz, H. Walter, "Moderne Schwingfestigkeitsnterlage
# fuer die Bemessung von Bauteilen aus Sphoeroguss und Temperguss- Teil 1
# ATZ Automobile Zeitschrift 86 1984 7/8 pp.325-331.
# Some specimens are Rotating Bending with Kt=1.1
# Ref.2: A.Fatemi, J.Williams,F.Montazersadgh, "Fatigue Performance Evaluation
# of Forged Steel versus Ductile Cast Iron Crankshaft: A Comparative Study,"
# U.of Toledo Report, Aug. 2007.
#
#FileType= strain_life
#DataType= fitted
#TIMEcol= 0
#NAME=  GGG60
#NAME=  80.55.06
#NAME=  NodularIron
#Stress_units= mpa
#Strain_units= strain
#Sy= 401   average
#Su= 638   average
#eu= 0.05
#E= 166000  average
#FractureStrain= 0.065 average
#FractureStress= 724   average
#BHN= 215  ave.
#%RA= 6.4  ave.
#saedigcurve_v2.2.f starts.
#
#NOTE!! The Following Points are <b>FITTED DATA:</b>#NOTE!! Fitted Stress computed using Experm. K' and n'
#StrAmpl     2Nf  StsAmpl So  PlasStrAmpl IniMod   NeuberStressAmpl
    .07             1   618        0     .06       166000. #Fitted_point monotonic
   0.00860        340   507.1      0.   0.00539    166000. #Fitted_point
   0.00644        785   486.8      0.   0.00335    166000. #Fitted_point
   0.00503       1520   467.1      0.   0.00208    166000. #Fitted_point
   0.00388       3460   441.7      0.   0.00109    166000. #Fitted_point
   0.00333       6000   422.6      0.   0.00065    166000. #Fitted_point
   0.00293      10800   403.5      0.   0.00038    166000. #Fitted_point
   0.00257      22600   377.8      0.   0.00018    166000. #Fitted_point
   0.00236      50000   358.1      0.   0.00010    166000. #Fitted_point
   0.00219      90000   338.8      0.   0.00005    166000. #Fitted_point
   0.00201     180000   314.4      0.   0.00002    166000. #Fitted_point
   0.00189     400000   297.2      0.   0.00001    166000. #Fitted_point
   0.00178    1000000   281.0      0.   0.00001    166000. #Fitted_point
   0.00151    6800000   251        0     0         166000. #Fitted_point manually
#Not clear if there is a flat fatigue limit.

#

#MagFactor= # Enter your Strain Reversal Points:

Simulate:

#TOTDAM(SWT)=  0.0000000E+00 allowed Repeats=      inf   nrev=         1