The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of testspecimen 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 000.50520.2001950023100.00220.50520.20019511538.77130.001146400.00440.50520.20019523177.44540.002269500.00660.50520.20019534716.21680.003392900.00880.50520.20019546404.84230.0044116000.0110.50520.20019557943.61360.0055130000.0150.50520.20019564936.80840.0075140000.020.50520.20019569931.94750.01144000.0250.50520.20019571930.00310.0125145000.060.50520.20019572429.5170.03146000.080.50520.20019572929.03090.04148000.10.50520.20019573928.05880.05146000.120.50520.20019572929.03090.0613600Fracture0.50520.20019567933.8918Fracture

Following is the graph deduced from the given information in the table: Part a. Proportional…

Answered: The following data were obtained from…

Steel Design (Activate Learning with these NEW titles from Engineering!)

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Author:Segui, William T.

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Chapter1: Introduction

Section: Chapter Questions

Problem 1.5.6P: The data in Table 1.5.3 were obtained from a tensile test of a metal specimen with a rectangular...

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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

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