elongation characteristics tabulated below to complete parts (a) through (f).

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
icon
Related questions
Question
Example
A cylindrical specimen of aluminum having a diameter of 0.505 in. (12.8 mm) and
a gauge length of 2.000 in. (50.800 mm) is pulled in tension. Use the load-
elongation characteristics tabulated below to complete parts (a) through ().
Load
Length
Ib
in.
(a) Plot the data as engineering stress
50.800
2.000
7,330
1,650
50.851
2.002
versus engineering strain.
15,100
3,400
50.902
2.004
(b) Compute the modulus of elasticity.
23,100
5,200
50.952
2.006
30,400
6,850
51.003
2.008
(c) Determine the yield strength at a strain
34,400
7,750
51.054
2.010
offset of 0.002.
38,400
8,650
51.308
2.020
41,300
9.300
51.816
2.040
(d) Determine the tensile strength of this
44,800
10,100
52.832
2.080
46,200
10,400
53.848
2.120
alloy.
47,300
10,650
54.864
2.160
(e) What is the approximate ductility, in
47,500
10,700
55.880
2.200
46,100
10,400
percent elongation?
56.896
2.240
44,800
10,100
57.658
2.270
) Compute the modulus of resilience.
WILEY
Chapter 8- 51
42,600
9,600
58.420
2.300
36,400
8,200
59.182
2.330
Fracture
Transcribed Image Text:Example A cylindrical specimen of aluminum having a diameter of 0.505 in. (12.8 mm) and a gauge length of 2.000 in. (50.800 mm) is pulled in tension. Use the load- elongation characteristics tabulated below to complete parts (a) through (). Load Length Ib in. (a) Plot the data as engineering stress 50.800 2.000 7,330 1,650 50.851 2.002 versus engineering strain. 15,100 3,400 50.902 2.004 (b) Compute the modulus of elasticity. 23,100 5,200 50.952 2.006 30,400 6,850 51.003 2.008 (c) Determine the yield strength at a strain 34,400 7,750 51.054 2.010 offset of 0.002. 38,400 8,650 51.308 2.020 41,300 9.300 51.816 2.040 (d) Determine the tensile strength of this 44,800 10,100 52.832 2.080 46,200 10,400 53.848 2.120 alloy. 47,300 10,650 54.864 2.160 (e) What is the approximate ductility, in 47,500 10,700 55.880 2.200 46,100 10,400 percent elongation? 56.896 2.240 44,800 10,100 57.658 2.270 ) Compute the modulus of resilience. WILEY Chapter 8- 51 42,600 9,600 58.420 2.300 36,400 8,200 59.182 2.330 Fracture
Expert Solution
steps

Step by step

Solved in 3 steps with 3 images

Blurred answer
Knowledge Booster
Types of Properties of Engineering Materials
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.
Similar questions
  • SEE MORE QUESTIONS
Recommended textbooks for you
Elements Of Electromagnetics
Elements Of Electromagnetics
Mechanical Engineering
ISBN:
9780190698614
Author:
Sadiku, Matthew N. O.
Publisher:
Oxford University Press
Mechanics of Materials (10th Edition)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:
9780134319650
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Thermodynamics: An Engineering Approach
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:
9781259822674
Author:
Yunus A. Cengel Dr., Michael A. Boles
Publisher:
McGraw-Hill Education
Control Systems Engineering
Control Systems Engineering
Mechanical Engineering
ISBN:
9781118170519
Author:
Norman S. Nise
Publisher:
WILEY
Mechanics of Materials (MindTap Course List)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:
9781337093347
Author:
Barry J. Goodno, James M. Gere
Publisher:
Cengage Learning
Engineering Mechanics: Statics
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:
9781118807330
Author:
James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:
WILEY