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# AISI-16MnCr5 Q+T Simulated Carburized Core, Iter.187 HRc=40.9 # NOTE!! 4Pt. Bending specimen ! Stroke(calibrated to Strain) control # 100% Matensite # Gerdau Ht.M54353 ElecFurn, VacDegas LadleRefine HotRoll to 31mm bar # Rectangular bending specimen, polished to 600 grit surface. # Chem.: 0.16wt%C 1.22Mn .018P .034S .07Si .23Cu .1Ni 1.06Cr # .04Mo .002V .002Nb .02Al .01Sn # Stress is elastic computed bending strress = Mc/I # M= (P/2)*2 inch-lbs, c=0.124in I=0.00065104 in^4 # Subsurface failures not seen in any fract. surfaces but multiple # initiation sites on surface apparent. # Tested by D.Gaia UWaterloo Aug.2016 #FileType= strain_life #DataType= raw #Name= 16MnCr5 #Name= Iter.187 #Name= SimulCore #Units= MPa #E= 201000 very approximate Emod #FailureDef= 50% load drop #Hardness, Brinell= 380 #Hardness, Rockwell C= 40.9 #BHN= 381 #Stress is elastic computed bending strress = Mc/I #M= (P/2)*2 inch-lbs, c=0.124in I=0.00065104 in^4 #Emod is simply StressAmpl/StrainAmpl #StrAmpl 2Nf StsAmpl-mpa So Sts/Str 0.00605 14882 1192 0 0 196991 0.00487 52372 970 0 0 199241 0.00448 70890 909 0 0 202933 0.00713 6960 1375 0 0 192888 0.00398 151726 803 0 0 201849 0.00348 135370 711 0 0 204257 0.00359 183318 717 0 0 199843 0.00317 192448 630 0 0 198672 0.00301 1666812 600 0 0 199336 0.00278 2000000 565 0 0 203351 #runout 0.00608 14940 1185 0 0 194930 #retest after runout 0.00280 2000000 560 0 0 200149 #runout 0.00710 6706 1370 0 0 192995 #retest after runout 0.00301 2000000 605 0 0 201008 #runout 0.00710 7288 1367 0 0 192547 #retest after runout 0.00500 52374 979 0 0 195703 0.00320 2000000 636 0 0 198878 #runout 0.00320 913794 638 0 0 199375 0.00598 13966 1188 0 0 198744 0.00451 82314 903 0 0 200115 0.00278 2000000 557 0 0 200398 #runout 0.00960 1587 1521 0 0 158416 0.00960 1710 1565 0 0 163063 0.00960 1763 1567 0 0 163229 #Carbon, %= 0.16 #Manganese, %= 1.22 #Phosphorus, %= 0.018 #Sulfur, %= 0.034 #Silicon, %= 0.07 #Copper, %= 0.23 #Nickel, %= 0.11 #Chromium, %= 1.06 #Molybdenum, %= 0.04 #Vanadium, %= 0.002 #Columbium/Niobium, %= 0.002 #Aluminum, %= 0.02 #Tin, %= 0.010 # #