SAE Standard Data File format

#SAE Standard Data File format #

Pick one: #FDE_plot #FDE_fit #
#

<pre>
#All of the data below was derived, but not copied, from the NASA Tech.
#Notes D-1574, D7532. The derivations and additions have been made 
#by the members of the FD&E committee of the SAE. Thus:
#
#Copyright (C) 2003,2012  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 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
#
# Merged file of three data sets:
# AA2014-T6 Aluminum, WROUGHT LONGITUDINAL, SMITH et al,NASA TN D-1574,1963
#     BHN 150/160
# AA 2014-T6 Aluminum, LONGITUDINAL, NACHTIGALL, NASA TN D-7532,FEB74
#     ASSUMED BHN 135
# AA 2014-T6, Ramusat+Vidal, Mem. Sci. Rev. Met. Jan 1979
#FileType= strain_life
#DataType= raw
#TIMEcol= 0
#NAME= AA2014-T6 
#NAME= merged 
#NAME= Aluminum
#Stress_units= ksi
#Strain_units= strain
#Sy=    70.4   #ksi average
#Su=    77.5   #ksi average
#E=    10520.  #ksi average
#%RA=   0
#BHN= 145.     #average
#NO. FAT. PTS.=  36
#Tot Strain      2Nf  Stress  Mean   Pl_Strain   Initial
#_ Amp                  Amp   Stress    Amp      Elastic Mod.
  0.033700        84.  77.45    0.  0.024900        9993.
  0.016400       406.  70.92    0.  0.009300        9993.
  0.010200      1216.  63.53    0.  0.003800        9993.
  0.006800      3220.  58.45    0.  0.001000        9993.
  0.006800      3960.  58.45    0.  0.001000        9993.
  0.005400      8360.  53.52    0.  0.000100        9993.
  0.003600    123400.  35.97    0.  0.000000        9993.
  0.004600    191100.  45.98    0.  0.000000        9993.
  0.003100    458000.  31.04    0.  0.000000        9993.
  0.003300    570000.  33.50    0.  0.000000        9993.
  0.002900    788000.  29.01    0.  0.000000        9993.
  0.002900    836000.  29.01    0.  0.000000        9993.

0.042850        22.  85.86    0.  0.034900       10791.
  0.022750        80.  83.69    0.  0.015000       10791.
  0.014650       224.  80.06    0.  0.007250       10791.
  0.014650       230.  80.21    0.  0.007200       10791.
  0.011550       460.  77.31    0.  0.004400       10791.
  0.008400      1330.  73.24    0.  0.001700       10791.
  0.005050     33040.  54.39    0.  0.000000       10791.
  0.003750    148120.  47.57    0.  0.000000       10791.
  0.003600    154400.  38.58    0.  0.000000       10791.
#below is from Ramusat/Vidal:
 0.02135    71    87.4    0    0.01363    10783
 0.01730    125    82.1    0    0.00978    10783
 0.01437    204    86.1    0    0.00660    10783
 0.01300    346    92.5    0    0.00457    10783
 0.01136    427    90.2    0    0.00353    10783
 0.01042    450    84.8    0    0.00273    10783
 0.00944    653    81.7    0    0.00201    10783
 0.00865    854    84.7    0    0.00110    10783
 0.00793    1328    77.6    0    0.00088    10783
 0.00802    1440    78.5    0    0.00062    10783
 0.00735    2249    76.5    0    0.00040    10783
 0.00649    3053    71.9    0    0.00018    10783
 0.00657    3430    72.8    0    0.00020    10783
 0.00648    4481    71.8    0    0.00015    10783
 0.00632    6499    67.5    0    0.00007    10783
#Here is the bottom part of the html  graph/calc wrapper:
#