A tension test on an aluminum alloy specimen produced the following load versus deformation data. The specimen was a 12 inch long bar with a diameter of 0.5 inches. The extensometer used to measure the deformation had a gage length of 4 inches. Use this data to answer questions 3.1-3.3. Table 3.2: Data for Problems 3.1-3.2 data point Deformation (in.) Load (lbs.) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 0.0005 0.0040 0.0075 0.0100 0.0125 0.0150 0.0175 0.0200 0.0225 0.0250 0.0275 0.0300 0.0325 0.0350 0.0375 0.0400 0.0425 0.0450 197 1565 2950 3923 4824 5890 6870 7540 7885 7990 8055 8080 8090 8120 8145 8155 8095 7880 3.1. Plot the stress-strain diagram for the test specimen. Use Excel or any appropriate software to create your graph.
A tension test on an aluminum alloy specimen produced the following load versus deformation data. The specimen was a 12 inch long bar with a diameter of 0.5 inches. The extensometer used to measure the deformation had a gage length of 4 inches. Use this data to answer questions 3.1-3.3. Table 3.2: Data for Problems 3.1-3.2 data point Deformation (in.) Load (lbs.) 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 0.0005 0.0040 0.0075 0.0100 0.0125 0.0150 0.0175 0.0200 0.0225 0.0250 0.0275 0.0300 0.0325 0.0350 0.0375 0.0400 0.0425 0.0450 197 1565 2950 3923 4824 5890 6870 7540 7885 7990 8055 8080 8090 8120 8145 8155 8095 7880 3.1. Plot the stress-strain diagram for the test specimen. Use Excel or any appropriate software to create your graph.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
Related questions
Question
Please answer complete question
Transcribed Image Text:3.11 Problems
A tension test on an aluminum alloy specimen produced the following load
versus deformation data. The specimen was a 12 inch long bar with a
diameter of 0.5 inches. The extensometer used to measure the deformation
had a gage length of 4 inches. Use this data to answer questions 3.1-3.3.
Table 3.2: Data for Problems 3.1-3.2
data point Deformation (in.) Load (lbs.)
1
2
3
4
5
6
7
TEET600
8
10
11
12
13
14
15
16
171
18
ARIA
0.0005
0.0040
0.0075
0.0100
0.0125
0.0150
a. Elastic modulus
b. Ultimate strength
C.
Modulus of resilience
d. Modulus of toughness
0.0175
0.0200
0.0225
0.0250
0.0275
0.0300
0.0325
0.0350
0.0375
0.0400
0.0425
0.0450
197
1565
2950
3923
4824
5890
6870
7540
85
7990
8055
8080
8090
8120
8145
8155
8095
7880
3.1. Plot the stress-strain diagram for the test specimen. Use Excel or any
appropriate software to create your graph.
3.2. Using the data of Table 3.2, along with your stress-strain plot, deter-
mine the following quantities:
Expert Solution
This question has been solved!
Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.
This is a popular solution!
Trending now
This is a popular solution!
Step by step
Solved in 3 steps with 2 images
Knowledge Booster
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, civil-engineering and related others by exploring similar questions and additional content below.Recommended textbooks for you
Structural Analysis (10th Edition)
Civil Engineering
ISBN:
9780134610672
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Principles of Foundation Engineering (MindTap Cou…
Civil Engineering
ISBN:
9781337705028
Author:
Braja M. Das, Nagaratnam Sivakugan
Publisher:
Cengage Learning
Structural Analysis (10th Edition)
Civil Engineering
ISBN:
9780134610672
Author:
Russell C. Hibbeler
Publisher:
PEARSON
Principles of Foundation Engineering (MindTap Cou…
Civil Engineering
ISBN:
9781337705028
Author:
Braja M. Das, Nagaratnam Sivakugan
Publisher:
Cengage Learning
Fundamentals of Structural Analysis
Civil Engineering
ISBN:
9780073398006
Author:
Kenneth M. Leet Emeritus, Chia-Ming Uang, Joel Lanning
Publisher:
McGraw-Hill Education
Traffic and Highway Engineering
Civil Engineering
ISBN:
9781305156241
Author:
Garber, Nicholas J.
Publisher:
Cengage Learning