Answer the following: a, b, c, d, e, f.Thank you! A specimen of magnesium having a rectan-gular cross section of dimensions 3.2 mm x19.1 mm in. × in.) is deformed in ten-sion. Using the load-elongation data tabulatedas follows, complete parts (a) through (f).lbf0310625126516701830222028903170322531102810LoadN013802780563074308140987012,85014,10014,34013,83012,500in.2.5002.5012.5022.5052.5082.5102.5252.5752.6252.6752.7252.775FractureLengthmm63.5063.5363.5663.6263.7063.7564.1465.4166.6867.9569.2270.49(a) Plot the data as engineering stress versusengineering strain.(b) Compute the modulus of elasticity.(c) Determine the yield strength at a strainoffset of 0.002.(d) Determine the tensile strength of this alloy.(e) Compute the modulus of resilience.(f) What is the ductility, in percent elongation?

As per the Bartelby answering guidelines we are supposed to answer first 3 sun parts of the…

Answered: (a) Plot the data as engineering stress…

(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.

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

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Concept explainers

Thermal Properties of Materials

In mechanical engineering, the thermal property is represented as the physical quantity that is relevant to the application of heat. The thermal properties are evaluated by variations in any specific material due to low heat or high heat. The quantities that influence the thermal property of the materials are mass, density, temperature, and many others.

Question

Answer the following: a, b, c, d, e, f.

Thank you!

A specimen of magnesium having a rectan-
gular cross section of dimensions 3.2 mm x
19.1 mm in. × in.) is deformed in ten-
sion. Using the load-elongation data tabulated
as follows, complete parts (a) through (f).
lbf
0
310
625
1265
1670
1830
2220
2890
3170
3225
3110
2810
Load
N
0
1380
2780
5630
7430
8140
9870
12,850
14,100
14,340
13,830
12,500
in.
2.500
2.501
2.502
2.505
2.508
2.510
2.525
2.575
2.625
2.675
2.725
2.775
Fracture
Length
mm
63.50
63.53
63.56
63.62
63.70
63.75
64.14
65.41
66.68
67.95
69.22
70.49
(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) Compute the modulus of resilience.
(f) What is the ductility, in percent elongation?

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