The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of test specimen was 0.505 inch and gauge length was 2.0 inch. Plot the stress strain diagram and determine (a) Proportional Limit (b) Modulus of Elasticity (c) Yield Stress at 0.2% offset (d) Ultimate Stress and (e) Nominal Rupture Stress. Load (lb) Elongation (in.) Initial Dia d1 (in.) Guage Length L1 (in.) Area (in2) Stress (psi) Strain 0 0 0.505 2 0.200195 0 0 2310 0.0022 0.505 2 0.200195 11538.7713 0.0011 4640 0.0044 0.505 2 0.200195 23177.4454 0.0022 6950 0.0066 0.505 2 0.200195 34716.2168 0.0033 9290 0.0088 0.505 2 0.200195 46404.8423 0.0044 11600 0.011 0.505 2 0.200195 57943.6136 0.0055 13000 0.015 0.505 2 0.200195 64936.8084 0.0075 14000 0.02 0.505 2 0.200195 69931.9475 0.01 14400 0.025 0.505 2 0.200195 71930.0031 0.0125 14500 0.06 0.505 2 0.200195 72429.517 0.03 14600 0.08 0.505 2 0.200195 72929.0309 0.04 14800 0.1 0.505 2 0.200195 73928.0588 0.05 14600 0.12 0.505 2 0.200195 72929.0309 0.06 13600 Fracture 0.505 2 0.200195 67933.8918 Fracture
The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of test specimen was 0.505 inch and gauge length was 2.0 inch. Plot the stress strain diagram and determine (a) Proportional Limit (b) Modulus of Elasticity (c) Yield Stress at 0.2% offset (d) Ultimate Stress and (e) Nominal Rupture Stress. Load (lb) Elongation (in.) Initial Dia d1 (in.) Guage Length L1 (in.) Area (in2) Stress (psi) Strain 0 0 0.505 2 0.200195 0 0 2310 0.0022 0.505 2 0.200195 11538.7713 0.0011 4640 0.0044 0.505 2 0.200195 23177.4454 0.0022 6950 0.0066 0.505 2 0.200195 34716.2168 0.0033 9290 0.0088 0.505 2 0.200195 46404.8423 0.0044 11600 0.011 0.505 2 0.200195 57943.6136 0.0055 13000 0.015 0.505 2 0.200195 64936.8084 0.0075 14000 0.02 0.505 2 0.200195 69931.9475 0.01 14400 0.025 0.505 2 0.200195 71930.0031 0.0125 14500 0.06 0.505 2 0.200195 72429.517 0.03 14600 0.08 0.505 2 0.200195 72929.0309 0.04 14800 0.1 0.505 2 0.200195 73928.0588 0.05 14600 0.12 0.505 2 0.200195 72929.0309 0.06 13600 Fracture 0.505 2 0.200195 67933.8918 Fracture
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
Related questions
Question
The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of test
specimen was 0.505 inch and gauge length was 2.0 inch. Plot the stress strain diagram and determine
(a) Proportional Limit (b) Modulus of Elasticity (c) Yield Stress at 0.2% offset (d) Ultimate Stress and
(e) Nominal Rupture Stress.
| Load (lb) | Elongation (in.) | Initial Dia d1 (in.) | Guage Length L1 (in.) | Area (in2) | Stress (psi) | Strain |
| 0 | 0 | 0.505 | 2 | 0.200195 | 0 | 0 |
| 2310 | 0.0022 | 0.505 | 2 | 0.200195 | 11538.7713 | 0.0011 |
| 4640 | 0.0044 | 0.505 | 2 | 0.200195 | 23177.4454 | 0.0022 |
| 6950 | 0.0066 | 0.505 | 2 | 0.200195 | 34716.2168 | 0.0033 |
| 9290 | 0.0088 | 0.505 | 2 | 0.200195 | 46404.8423 | 0.0044 |
| 11600 | 0.011 | 0.505 | 2 | 0.200195 | 57943.6136 | 0.0055 |
| 13000 | 0.015 | 0.505 | 2 | 0.200195 | 64936.8084 | 0.0075 |
| 14000 | 0.02 | 0.505 | 2 | 0.200195 | 69931.9475 | 0.01 |
| 14400 | 0.025 | 0.505 | 2 | 0.200195 | 71930.0031 | 0.0125 |
| 14500 | 0.06 | 0.505 | 2 | 0.200195 | 72429.517 | 0.03 |
| 14600 | 0.08 | 0.505 | 2 | 0.200195 | 72929.0309 | 0.04 |
| 14800 | 0.1 | 0.505 | 2 | 0.200195 | 73928.0588 | 0.05 |
| 14600 | 0.12 | 0.505 | 2 | 0.200195 | 72929.0309 | 0.06 |
| 13600 | Fracture | 0.505 | 2 | 0.200195 | 67933.8918 | Fracture |
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 2 steps with 1 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