hello i hope you are fineI need your help by solving the question below. Please, please, please quickly,because I am studying now and I have exams in the coming days, so I need to do this homework in order to understand the study material and I do not have much time. I need to solve within half an hour or a little more.please please please B/ The following data were collected from a test specimen of cold-rolled and annealed brass.The specimen had an initial gage length Lo of (35 mm )and an initial cross-sectional area A,of (10.5 mm?).Load (N) 0.0241025.25663274627971.72135017208.15222013.072690177AL (mm) 0.0 0.0112 0.0157 0.075 0.1995.5522.77Plot the engineering stress-strain curve and the true stress-strain curve. Since the instantaneouscross-sectional area of the specimen is unknown past the point of necking, truncate the truestress-true strain data at the point that corresponds to the ultimate tensile strength, and calculatethe following(a) The 0.2% offset yield strength;(b) The tensile strength;(c) The modulus of elasticity;(d) The % elongation;(e) The modulus of resilience.

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Answered: B/ The following data were collected…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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hello i hope you are fine
I need your help by solving the question below. Please, please, please quickly,
because I am studying now and I have exams in the coming days, so I need to do this homework in order
to understand the study material and I do not have much time. I need to solve within half an hour or a little more.please please please

B/ The following data were collected from a test specimen of cold-rolled and annealed brass.
The specimen had an initial gage length Lo of (35 mm )and an initial cross-sectional area A,
of (10.5 mm?).
Load (N) 0.0
2410
25.25
66
327
462
797
1.72
1350
1720
8.15
2220
13.07
2690
177
AL (mm) 0.0 0.0112 0.0157 0.075 0.199
5.55
22.77
Plot the engineering stress-strain curve and the true stress-strain curve. Since the instantaneous
cross-sectional area of the specimen is unknown past the point of necking, truncate the true
stress-true strain data at the point that corresponds to the ultimate tensile strength, and calculate
the following
(a) The 0.2% offset yield strength;
(b) The tensile strength;
(c) The modulus of elasticity;
(d) The % elongation;
(e) The modulus of resilience.

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