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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.
- Fall '05