Material + Cycles File

#Material + Cycles File #

1. Your Material (Digital-Fitted Curves):


# NOTE!! Fitted Curve data !!
# SAE1552 Simul.Core  Induction  hardened  AISI Iter.94 HRc=24
# As-Rolled Simulated Induction Hardened Core
# MacSteel Monrow Heat M10473 ElecFurn LadleRef. Concast HorRolled 25.7mm bar
# Chem.: 0.52%C 1.43Mn .011P .012S .24Si .09Cu .09Ni .10Cr .01Mo
# .066V .001Nb .001Al .0001Pb .001Ti .01Co .0003B .005Sn 115pppm_N
# Axial Specimens machined, induction hardened, polished.
# Inclusion Rating      Type A (sulfide) 1.3T 0.1H Type B (alumina) 0.7T 0.0H
# Type C (silicate) 0.3T 0.0H Type D (globular) 0.8T 0.1H
# Pearlite 65% Ferrite 35% ASTM Grain Size No. (Min to Max)= 5 to 8
# Tested by A.A. Rteil Uwaterloo, 2006

#FileType= strain_life
#DataType= fitted
#Name= SAE1552
#Name= AisiIt_94
#Stress_units= MPa
#Strain_units= strain
#Sy= 420.0
#Su= 964.0
#E= 196000
#monotonic_K= 2127.0
#monotonic_n= 0.261
#MaterialForm= bar
#FailureDef= 50% load drop
#Hardness, Rockwell C= 24
#BHN= 247
#Original No. fatigue data points=   20
#
#NOTE!! The Following Points are <b>FITTED DATA:</b>
#NOTE!! Fitted Stress computed using Experm. K' and n'
#NOTE!! Manually adjusted Fatigue limit points.  FAC may09
#_Total Strain   2Nf  Stress  Mean   Plastic Strain   
#_   Amp               Amp   Stress      Amp        EMod.
   2.65316          1  1441.6      0.   2.64580    196000. #Fitted_point
   1.57570          2  1357.8      0.   1.56877    196000. #Fitted_point
   0.79255          5  1254.5      0.   0.78615    196000. #Fitted_point
   0.47219         10  1181.5      0.   0.46616    196000. #Fitted_point
   0.28211         20  1112.9      0.   0.27644    196000. #Fitted_point
   0.14381         50  1028.2      0.   0.13856    196000. #Fitted_point
   0.08713        100   968.4      0.   0.08219    196000. #Fitted_point
   0.05341        200   912.2      0.   0.04875    196000. #Fitted_point
   0.02875        500   842.8      0.   0.02445    196000. #Fitted_point
   0.01856       1000   793.9      0.   0.01451    196000. #Fitted_point
   0.01243       2000   747.8      0.   0.00861    196000. #Fitted_point
   0.00784       5000   690.9      0.   0.00432    196000. #Fitted_point
   0.00588      10000   650.8      0.   0.00256    196000. #Fitted_point
   0.00464      20000   612.8      0.   0.00151    196000. #Fitted_point
   0.00364      50000   565.7      0.   0.00075    196000. #Fitted_point
   0.00316     100000   532.1      0.   0.00044    196000. #Fitted_point
   0.00281     200000   500.3      0.   0.00026    196000. #Fitted_point
   0.00248     500000   460.6      0.   0.00013    196000. #Fitted_point
   0.00228    1000000   432.6      0.   0.00007    196000. #Fitted_point
   0.00211    2000000   406.2      0.   0.00004    196000. #Fitted_point
    .002      3000000   391.       0.   0.0        196000. #Fitted_point   Adjusted
    .002     10000000   391.       0.   0.0        196000. #Fitted_point   Adjusted

#

2. History Magnification or Multiplication factor

3. Enter Elastic Kt*Nominal (or Finite Element) Stress History (Rainflow counted cycle sets) Below:

MPa !

Cycle Set #1 : Smax Smin Cycles
Cycle Set #2 : Smax Smin Cycles
Cycle Set #3 : Smax Smin Cycles
Cycle Set #4 : Smax Smin Cycles
Cycle Set #5 : Smax Smin Cycles
Cycle Set #6 : Smax Smin Cycles

1. Your Material (Digital-Fitted Curves):

2. History Magnification or Multiplication factor

3. Enter Elastic Kt*Nominal (or Finite Element) Stress History (Rainflow counted cycle sets) Below:

4. (Page will be submitted to UoWaterloo Website)