A cylindrical specimen of stainless steel having a diameter of 12.8 mm (0.505 in.) and a gauge length of 50.800 mm (2.000 in.) is pulled in tension. Use the load-elongation characteristics shown in the following table to complete parts (a) through (f).
LoadN012,70025,40038,10050,80076,20089,10092,700102,500107,800119,400128,300149,700159,000160,400159,500151,500124,700Lengthlbf02,8505,7108,56011,40017,10020,00020,80023,00024,20026,80028,80033,65035,75036,00035,85034,05028,000mm50.80050.82550.85150.87650.90250.95251.00351.05451.18151.30851.56251.81652.83253.84854.35654.86455.88056.642in.2.0002.0012.0022.0032.0042.0062.0082.0102.0152.0202.0302.0402.0802.1202.1402.1602.2002.230
(a) Plot the data as engineering stress versus engineering strain.
(b) Compute the modulus of elasticity.
(c) Determine the yield strength at a strain offset of 0.002.
(d) Determine the tensile strength of this alloy.
(e) What is the approximate ductility, in percent elongation?
(i) Compute the modulus of resilience.