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Composite manufacturing and testing ENG 364 Materials Engineering Laboratory PRAC 2 - Tensile testing. Aim 1. To understand the behaviour of different materials under tension. 2. To determine the...

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Composite manufacturing and testing
ENG 364 Materials Engineering Laboratory
PRAC 2 - Tensile testing.
Aim
1. To understand the behaviour of different materials under tension.
2. To determine the following mechanical properties of metals:
· 0.1% Proof stress
· Ultimate Tensile Strength
· % elongation
· % reduction of area
· Young’s Modulus (Elastic Modulus)
· Elastic limit
3. From data draw conclusions about the material type.
4. Consolidate theory on dislocation movement, and strain hardening.
5. Visualize a material failure under a microscope.
Readings and Specification:
You must read the following Australian Standard before coming to the class. The standard can be accessed by going to the link http:
www.cdu.edu.au/li
ary/search/a-z_databases.html#A and using your student credentials for login. Only two students/staff can be logged on at the same time. Logout as soon as you have finished.
AS 1391, Metallic materials—Tensile testing at ambient temperature.
Things to consider:
You need to measure the load and extension of the sample undergoing tension.
Load is read off a load cell meter.
You need to measure the extension using a dial gauge.
The tensile test will be conducted on a bench-top tensile tester.
Recording
    Sample 1 -
    
    Sample 2 -
    
    Sample 3 -
    Force (kN)
    Î”
    
    Force (kN)
    Î”
    
    Force (kN)
    Î”
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
    
Post Test
7.
When the test piece fractures, remove the fractured pieces from the grips. Be careful not to erase your gauge marks.
8.
Place the fractured pieces together and measure the elongation between the gauge marks.
9.
Note the failure surface and view under a stereo microscope.
Calculations:
From the test results determine the mechanical properties.
· Yield stress or 0.1 % proof stress
· Ultimate Tensile Strength
· % elongation
· % reduction of area
· Young’s Modulus (Elastic Modulus)
On the stress strain curve indicate:
· Yield stress or 0.1 % proof stress
· Ultimate Tensile Strength
· Elastic limit
· Plastic region
Report Format: Not more than 4 pages
The report should contain:
· Date and Title
· Results, charts, discussion including comparison to theory, predictions and e
or
· Conclusions and suggestions for improvement.
· Answers to questions given below.
Questions
You must answer the following questions as well.
1. What determines the Young’s Modulus of materials?
2. If the yield strength of a material is increased three times by heat treatment, how many times will the elastic deflection increase for the same load?
3. If a material is loaded above yield strength but below ultimate tensile strength and unloaded, what will be its yield strength when reloaded? You could draw schematic diagram to illustrate this.
4. Name some typical uses for the materials tested based on your test results.
    Section
    Allocated marks
    Entry of data during the lab class
    20
    For the materials provided, calculate
Yield stress
Ultimate Tensile Strength
% elongation
% reduction of area
Young’s Modulus (Elastic Modulus)
    25
    Conclusions with suggestions for improvement
    15
    Answers to questions
    40
    
    TOTAL = 100

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Answered 2 days After Jun 21, 2021

Solution

Asif answered on Jun 24 2021
159 Votes
Running Head: ENG 364 MATERIALS ENGINEERING LABORATORY
    ENG 364 MATERIALS ENGINEERING LABORATORY
            9
ENG 364 MATERIALS ENGINEERING LABORATORY
DATE: 24.06.2021
Executive Summary
The present report has shed light on laboratory recordings from a tensile test of three different materials as Aluminium, Stainless Steel, and Galvanized Steel. Firstly, recording from lab results has been stated in a tabular form that has been successfully used to measure applied force and elongation of test materials. Furthermore, a detailed calculation of given test requirements has been detailed in this report. Drawings have taken place based on the given requirements of the report and a conclusion has been drawn based on overall report findings and discussions. Finally,
ief answers to the given questions have been added to this report.
Table of Contents
Recording    4
Calculations    4
Conclusion and Suggestions    6
Answers to Questions    6
References    9
Recording
    Sample 1- Aluminium
    Sample 2- Stainless Steel
    Sample 3- Galvanised Steel
    Force (kN)
    Î”
    Force (kN)
    Î”
    Force (kN)
    Î”
    0
    0
    0
    0
    0
    0
    7.5
    1.4
    2.9
    0.3
    9.4
    1.1
    7.9
    1.7
    5.7
    0.4
    11.6
    1.2
    8.0
    1.8
    9.6
    0.6
    12.8
    1.3
    8.1
    2.1
    15.8
    0.9
    14.1
    1.4
    8.2
    2.4
    19.3
    1.0
    14.2
    1.5
    8.3
    2.9
    22.9
    1.2
    14.3
    2.1
    Necking to Failure
    23.2
    1.4
    14.6
    2.7
    
    35.1
    6.2
    15.3
    9.7
    
    47.2
    22.4
    16
    12.7
Table 1: Recording from Laboratory
(Source: Created by Researcher)
Calculations
Yield Stress
The 0.2% Offset Rule will be applied for measuring the Yield Stress;
Assuming Yield Strain is 0.2% and multiplying it with Young’s Modulus of materials defines Yield Stress;
Therefore,
Yield Stress for Aluminium (σ) = 0.002*69 = 0.138
Yield Stress for Stainless Steel (σ) = 0.002*190 = 0.38
Yield Stress for Galvanized Steel (σ) = 0.002*200 = 0.4
Ultimate Tensile Strength
Assuming Critical Load (Pc) = m = 9.81 m/s2
UTS for Aluminium Sample
C/S Area of Aluminium Sample = 6*1.10 = 6.6 mm2
Therefore;
UTS = T = Pc/A = 9.81/6.6 = 1.48 GPa
UTS for Stainless Steel Sample
C/S Area of Stainless Steel Sample = 6*1.10 = 6.6 mm2
Therefore;
UTS = T = Pc/A = 9.81/6.6 = 1.48 GPa
UTS for Galvanized Steel Sample
C/S Area of Galvanized Steel Sample = 5.9*0.9 = 5.31 mm2
Therefore;
UTS = T = Pc/A = 9.81/6.6 = 1.85 GPa
% of Elongation
Where, ΔL = Final Length before Failure and L = Initial...
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