m16_ps05_spring04

m16_ps05_spring04 - 53.848 160400 54.356 159500 54.864...

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Unified Engineering Spring 2004 Problem M16 A cylindrical specimen of stainless steel having a diameter of 12.8 mm and a gauge length of 50.8 mm is pulled in tension. Use the load-elongation characteristics tabulated below to complete problems (a) through (f). Load (N) Length (mm) 0 50.800 12700 50.825 25400 50.851 38100 50.876 50800 50.902 76200 50.952 89100 51.003 92700 51.054 102500 51.181 107800 51.308 119400 51.562 128300 51.816 149700 52.832 159000
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Unformatted text preview: 53.848 160400 54.356 159500 54.864 151500 55.880 124700 56.642 FRACTURE a) Plot the data as engineering stress vs. engineering strain. b) Compute the Young's modulus c) Determine the yield strength at a strain offset of 0.002 (0.2%) d) Determine the tensile strength of this alloy e) What is the approximate ductility expressed as a percentage of elongation? f) Estimate the energy that must have been supplied to cause the specimen to reach failure....
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This note was uploaded on 01/28/2012 for the course AERO 16.01 taught by Professor Markdrela during the Fall '05 term at MIT.

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