Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering)
10th Edition
ISBN: 9780073398204
Author: Richard G Budynas, Keith J Nisbett
Publisher: McGraw-Hill Education
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Textbook Question
Chapter 1, Problem 16P
The tensile 0.2 percent offset yield strength of AISI 1137 cold-drawn steel bars up to 1 inch in diameter from 2 mills and 25 heats is reported as follows:
Sy | 93 | 95 | 97 | 99 | 101 | 103 | 105 | 107 | 109 | 111 |
f | 19 | 25 | 38 | 17 | 12 | 10 | 5 | 4 | 4 | 2 |
where Sy is the class midpoint in kpsi and f is the number in each class. Presuming the distribution is normal, what is the yield strength exceeded by 99 percent of the population?
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A 1045 hot-rolled steel tension test specimen has the original diameter and length of 6 mm
and 25 mm, respectively. The load and change in length data were recorded as shown in
Table 1 below:
Table 1. Load and change in length
Load (KN)
Change in Length Load (KN)
Change in Length
(mm)
(mm)
20.56
2.26
2.94
0.01
20.72
3.36
5.58
0.02
20.61
3.83
8.52
0.03
19.97
4.00
11.16
0.04
18.72
Fracture.
12.63
0.05
13.02
0.06
13.16
0.08
13.22
0.10
16.15
0.61
18.50
1.04
20.27
1.80
Page 16
3.1) Calculate stress and strain for the data in Table 1. Please show 1 calculation of stress
and 1 of strain. The rest you must tabulate.
Calculate the (total tensile strength) of the mitotic tensile strength test for the information in the table below:
Time
#
D mm
Load Kn
sec
1
60
16
14
2
54
15.5
14
3
57
16
15.5
4
52
15
18
5
53
15
14
59
17.5
19
50
9
17
56
19
21
58
10
21.4
55
11
25
67899
10
During a tensile test of Aluminum alloy whose initial diameter was 0.505-in and gage
length was 2.0-in, the following data was recorded.
Load
Elongation
(in.)
Load
Elongation
(in.)
0.020
(1b)
|(Ib)
14 000
2 310
0.00220
14 400
0.025
4 640
0.00440
14 500
0.060
6 950
0.00660
14 600
0.080
9 290
0.00880
14 800
0.100
11 600
0.0110
14 600
0.120
12 600
0.0150
13 600 Fracture
a) Determine Stress and strain
b) Draw the stress strain diagram
c) Determine the following mechanical properties
1) Proportional limit,
2) Modulus of elasticity
3) Yield point
4) Ultimate strength
5) Rupture strength.
Chapter 1 Solutions
Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering)
Ch. 1 - Select a mechanical component from Part 3 of this...Ch. 1 - Select a mechanical component from Part 3 of this...Ch. 1 - Select an organization listed in Sec. 16, go to...Ch. 1 - Go to the Internet and connect to the NSPE website...Ch. 1 - Go to the Internet and connect to the NSPE website...Ch. 1 - Estimate how many times more expensive it is to...Ch. 1 - The costs to manufacture a part using methods A...Ch. 1 - A cylindrical part of diameter d is loaded by an...Ch. 1 - When one knows the true values x1 and x2 and has...Ch. 1 - Use the true values x1 = 7 and x2 = 8 (a)...
Ch. 1 - A solid circular rod of diameter d undergoes a...Ch. 1 - A fatigue test is performed on rotating beam...Ch. 1 - Determinations of the ultimate tensile strength...Ch. 1 - The lives of parts are often expressed as the...Ch. 1 - The tensile 0.2 percent offset yield strength of...Ch. 1 - A mechanical system comprises three subsystems in...Ch. 1 - From See. 3-12, the maximum shear stress in a...Ch. 1 - A round cold-drawn 1045 steel rod has a mean...Ch. 1 - A beam subjected to axial loading will experience...Ch. 1 - Three blocks A, B, and C and a grooved block D...Ch. 1 - The volume of a rectangular parallelepiped is...Ch. 1 - A pivot in a linkage has a pin in the figure whose...Ch. 1 - A circular cross section O ring has the dimensions...Ch. 1 - Prob. 25PCh. 1 - Prob. 26PCh. 1 - Prob. 27PCh. 1 - Prob. 28PCh. 1 - Convert the following to appropriate ips units:...Ch. 1 - Convert the following to appropriate SI units: (a)...Ch. 1 - Generally, final design results are rounded to or...Ch. 1 - Repeal Prob. 1-31 for the following: (a) = F/wt,...Ch. 1 - Repeat Prob. 131 for: (a) = F/A, where A = d2/4, F...
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