AERO214 Axial Loading
docx
keyboard_arrow_up
School
Texas A&M University *
*We aren’t endorsed by this school
Course
214
Subject
Mechanical Engineering
Date
Dec 6, 2023
Type
docx
Pages
8
Uploaded by MasterWorld12545
Tension Test
INTRODUCTION Tensile testing is performed on materials to ascertain important mechanical properties like
Young’s modulus, tensile strength, yield strength, ductility and fracture strength. The
fundamental purpose of a tensile test is to determine the deformation response of a given
material under a specified load. This information is critical in the design of load carrying
structural members. Tensile tests are performed with specimens of various geometries. Often, a
specimen with a circular or flat rectangular cross section is used. In this laboratory experiment,
we will be using a flat rectangular configuration. OBJECTIVES • To understand how a tensile test is performed and how to obtain the relevant material properties
• To determine the following properties for given metallic specimens (Aluminum 6061, 316
Stainless Steel, and 1018 Carbon Steel) using a uniaxial tensile test: Young’s modulus, E Yield strength, σ
Tensile strength, Strain to failure Lab-Specific Information
Each lab group will conduct the experimental portion for the entirety of the lab, examining the
response of each of the three samples to tensile loading. Each group will be responsible for
writing a lab report due two weeks after the date the lab was conducted. Axial Loading:
This lab examines the elastic and plastic deformation of an axially-loaded material to failure.
Three separate materials are examined in this work. Each lab group is responsible for developing
stress-strain curves to obtain a deeper understanding of constitutive relationships, strain
hardening, strength, and failure. THEORY
Inputs: F
Measured Outputs: ∆ L
Calculated Outputs: ε
, E
Known Parameters: A, L, For a rod with gage length L with both ends fully constrained (no
translational or rotational movement allowed), the applied force can be
converted to stress by dividing the applied load by the cross-sectional
area:
L
σ
=
F
A
The axial strain ε
can be obtained – correlating the change in length of the sample (
∆ L
) to
the original gage length. ε
=
∆ L
L
The sample geometry shown in the shape is referred to as a dog bone sample. We use the gage
length (measured from the beginning of curvature of the sample) rather than the total length in
calculating the strain. This is because the deformation scales inversely with cross-sectional area:
The two “heads” of the sample experience much less strain than the gage length, and the strain in
the heads is considered to be negligible. A COUPLE OF KEY TERMS
The modulus of elasticity
: also known as the young’s modulus – can be obtained for an elastic
response of the material.
E
=
σ
ε
Elastic modulus does not use data from the plastic regime
or failure regime
of the stress-strain
curve.
Gage Length:
constant-radius section of experimental sample.
Necking: visible reduction in cross-sectional area in a sample at the point where failure is
imminent. Strain to failure:
The maximum strain that the sample can take right before rupture.
Yield stress:
The minimum stress required for the solid to undergo plastic deformation.
Energy to failure:
The energy per unit volume of the material required to break the sample. It is
equal to the area under the stress-strain curve.
TEST PROCEDURE
This lab examines three
separate materials:
Aluminum 2024
Aluminum 6061
ASTM-A36 Carbon Steel
For each material, begin by obtain the gage length and cross-sectional dimensions of each
sample. Each sample will be loaded to fracture in the INSTRON tensile testing apparatus, seen
below:
Figure 1: Instron Test Apparatus
The test methods for each of the tests below have already been programmed into the INSTRON
Bluehill software package. These methods will automatically output the force and deformation
data to an excel sheet, with a separate sheet for each run, which you can email to yourself for
data analysis.
Aluminum 6061 and 316 Stainless Samples ONLY: Loading to Fracture
1.
Position your sample in the test apparatus, zeroing the force and deformation gages or
readings
2.
Log in to the computer with your TAMU ID and password, then access the data folder on
the desktop window. Each run will store data to this folder. Open the Instron software
package on the desktop window. Upon opening, enter the userID and password provided
by the TA.
Your preview ends here
Eager to read complete document? Join bartleby learn and gain access to the full version
- Access to all documents
- Unlimited textbook solutions
- 24/7 expert homework help
3.
Upon opening the Instron software package, select the test tab. Select the first of the two
214 tensile test methods. Figure 2: Method Selection
4.
Ensure that the travel limits are set correctly for starting the test – make sure you have the
slides positioned so the sample can be loaded to failure, as well as positioned in the test
apparatus. Set the lower limit just below the start position. Use the jog up and jog down
buttons on the physical controller on the right side of the test apparatus to position the
grips and insert the test sample.
5.
Double-check with the TA to ensure your operator inputs are correct. Click zero
displacement, then balance force. This should position the sample in a zero-force state
where the sample is gripped but not loaded, as seen below. 6.
Hit start once the sample is in a zero-force state. The
method
will continue applying load and measuring the
deformation and applied force at regular increments.
This method will also pause periodically for you to
observe the sample, requiring manual input to
continue after the sample state has been observed.
7.
Once you see necking occur, carefully observe sample
failure over the next few mm of deformation and note
how the force vs deformation data changes as well as
the visual effects on the sample.
8.
Once fracture occurs, observe the fracture interface
and record notes on it.
9.
Record the length immediately prior to failure, or if possible, place the
fractured pieces together and use to measure the final gage length.
Figure 3: Slide
Limits
Figure 4: Gripped
Sample
1018 Carbon Sample ONLY: Strain Hardening
1.
Repeat steps 1-6 from the first two samples but change the test method to the second 214
214 test method. This method will examine strain hardening, where you will load a
material to the point where plastic deformation occurs, unload the material to a zero-force
state, then re-load to failure.
2.
When the sample reaches 13kN of force, the method will unload the sample, recording
force vs deflection to a zero-force state. (
A/N – your length will NOT go back to zero, you
have permanently deformed the sample via plastic deformation!)
3.
Note the new initial length of the sample. This is the new ‘base’ length of the plastically
deformed, strain-hardened sample.
4.
Continue execution of the method: the sample will be resubjected to an applied load until
fracture occurs. Note how the response of the material is different compared to the elastic
loading regime from earlier.
REPORTING REQUIREMENTS
Lab Content (50 Points)
For each material, plot stress vs strain for each of the tests conducted. For the steel
sample, plot stress vs strain for the initial loading, the unloading, and the re-loading to
failure, and clearly identify each. (10 points)
For each material, determine the modulus of elasticity using only the linear-elastic
portion of the graph. Keep track of units, and either show in graphs or calculations how
your modulus was obtained. Calculate the uncertainty of the modulus (7.5 points)
What does an R
2
value represent for linear regression? Define and explain your elastic
regime, plastic regime, and failure regime for each plot, as well as your yield and ultimate
strengths (7.5 points)
Briefly comment on what the boundary conditions for this test setup would be, and draw
a free body diagram for the test (5 points)
Compare the calculated values of modulus of elasticity (with uncertainty) to those from
the literature and comment on the accuracy of the results. (5 points)
Calculate and record the yield strength, tensile strength, fracture stress, ductility, and
toughness for all specimens. Compare this to published data. Calculate uncertainty for
each value and report results with correct significant figures (10 points)
Show sample calculations for all the data in steps 5 and 6 for one of the samples in an
appendix. Clearly state the equations used for each calculation and show step-by-step
calculations. (10 points)
Discuss how strain hardening affected the material properties of the steel sample, clearly
showing how plastically deforming the material impacted properties such as elasticity,
yield strength, and ductility. (5 points)
Lab Report (50 points)
Title Page:
(2.5 points)
The cover page should provide the following information: Report Title, Report Authors
(Team Number, UINs, and Team Leader(s) if any for the report), Date Conducted, Date
Submitted.
Templates are available through Texas A&M
Table of Contents:
(2.5 points)
Includes and hyperlinks all sections of the report – for each section you should have intro,
abstract, conclusions, and all other sections listed.
Includes and hyperlinks figures, tables, and appendices
Abstract:
(7.5 points)
Your preview ends here
Eager to read complete document? Join bartleby learn and gain access to the full version
- Access to all documents
- Unlimited textbook solutions
- 24/7 expert homework help
This summarizes (1) what the purpose of the lab is, (2) what concepts are covered, (3)
what was done in the lab, (4) what results were obtained (include quantitative
information!), and (5) why these results are important.
Your report should be written such that someone who has not done the lab or who does
not have prior knowledge of the lab should be able to understand what you did, why you
did it, what data you obtained, and why it matters!
Introduction:
(10 points)
This section details the motivation, background, and theory of the lab.
Make sure you clearly explain the motivation for the experiment – why does it matter?
Why does it have value? What is the background of the lab? Why are you conducting this
lab?
Make sure you adequately summarize the experiment here! This is separate from the
experimental procedure, which is a step-by-step writeup of the steps you took.
Make sure you clearly define
all equations, terms, and variables. All of these should be
defined! Experimental Procedure:
(5 points)
This section is a step-by-step writeup of the experimental procedure you used to conduct
the lab
This must
be in your own words!
Data and Results:
(10 points)
This section is primarily tables – both of the raw data (which can be placed in an
appendix, and probably should be for most labs for readability!) and the calculated data.
This section will also include the lab content requested for each lab.
Make sure your data is readable
and directly included (no google sheets links). If you
directly import handwritten data, be very careful that your work is legible and is as clear
as typed work would be.
Include uncertainty and track your significant figures!
Be careful with figure formatting – units, titles, error bars, axes, etc. This matters
significantly
when it comes to good reports!
Discussion and Conclusions (
10
points)
Discussion: discuss the results obtained – do they seem reasonable? Are there any
calculations where you know your results are likely inaccurate? Do any figures need
axes, uncertainty, or any content explained? o
How closely do your calculated results line up to theory or expected results? o
What were the likely causes of error in your calculated results? Don’t just say
human error, need detail here!
Discussion and Conclusions (2.5 points)
Highlight important results. Include your conclusions on the lab and your results. Discuss
positive aspects of the lab (what went well, what worked) and any things that should be
changed for next semester or next lab.
Related Documents
Related Questions
I need the answer as soon as possible
arrow_forward
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.
arrow_forward
The following stress-strain curve was prepared based on a tensile test of a specimen that had a circular cross-section. The gage
diameter of the specimen was 0.25 inches and the gage length was 4 inches. The stress scale of the stress-strain diagram is
given with the factor a = 10 ksi. Estimate:
(a) The modulus of elasticity.
(b) The ultimate strength.
(c) The yield strength (0.2% offset).
(d) The percent elongation at fracture.
2013 Michael Swanbom
STRESS VS. STRAIN
BY NC SA
7a
bat
Sat
2at
at
0.05
STRAIN
0.01
0.04
0.06
0.08
0.02
0.03
0.07
0.09
STRESS
arrow_forward
The results of a tensile test are:
Diameter of the specimen
Gauge length
Load at limit of Proportionality
Extension at the limit of Proportionality
Maximum Load
: 10mm
:40 mm
: 70kN
:0.08mm.
:100 kN
Calculate stress at limit of proportionality and young's modulus.
arrow_forward
1. A tensile test was conducted on a metal "505" specimen and the following stress-strain curves
were generated, both curves generated from the same set of data. Use the graphs to fill in the
mechanical properties of the material tested in the box below. Don't forget units!
Stress vs Strain
Stress, psi
Stress, psi
80000
70000
60000
50000
40000
30000
20000
10000
0
0.00
80000
70000
60000
50000
40000
30000
20000
10000
0.02
0
0.000 0.002
0.04
0.004
0.06
0.006
0.08
0.10
Strain
Stress vs Strain
0.008
0.12
Elastic Modulus, E:
0.2% Offset Yield Strength, oo:
Tensile Strength, ou:
Breaking Strength, of:
% Elongation:
0.14
0.010 0.012 0.014
Strain
0.16
0.18
0.016 0.018
0.20
0.020
arrow_forward
I just can't find The percent elongation at fracture.
arrow_forward
Hello, I hope you are fine. I need to do this homework in Metal Engineering. I hope to get your help because I have an important homework.
arrow_forward
A tensile test was performed on a metal specimen with a diameter of
1/2 inch and a gage length (the length over which the elongation is meas-
ured) of 4 inches. The data were plotted on a load-displacement graph,
P vs. AL. A best-fit line was drawn through the points, and the slope of
the straight-line portion was calculated to be P/AL = 1392 kips/in. What
is the modulus of elasticity?
BI
arrow_forward
Draw a typical stress vs strain tensile test curve for the following material and label the axis.
A typical brittle material subjected to a tensile stress that has been applied to the material till the sample breaks.
1- label the axis and draw the curve for a brittle material.
2- indicate the maximum strength of the material.
3- show on the portion of the curve where young's modulus can be calculated.
arrow_forward
SEE MORE QUESTIONS
Recommended textbooks for you

Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press

Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON

Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education

Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY

Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning

Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY
Related Questions
- I need the answer as soon as possiblearrow_forwardThe 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.arrow_forwardThe following stress-strain curve was prepared based on a tensile test of a specimen that had a circular cross-section. The gage diameter of the specimen was 0.25 inches and the gage length was 4 inches. The stress scale of the stress-strain diagram is given with the factor a = 10 ksi. Estimate: (a) The modulus of elasticity. (b) The ultimate strength. (c) The yield strength (0.2% offset). (d) The percent elongation at fracture. 2013 Michael Swanbom STRESS VS. STRAIN BY NC SA 7a bat Sat 2at at 0.05 STRAIN 0.01 0.04 0.06 0.08 0.02 0.03 0.07 0.09 STRESSarrow_forward
- The results of a tensile test are: Diameter of the specimen Gauge length Load at limit of Proportionality Extension at the limit of Proportionality Maximum Load : 10mm :40 mm : 70kN :0.08mm. :100 kN Calculate stress at limit of proportionality and young's modulus.arrow_forward1. A tensile test was conducted on a metal "505" specimen and the following stress-strain curves were generated, both curves generated from the same set of data. Use the graphs to fill in the mechanical properties of the material tested in the box below. Don't forget units! Stress vs Strain Stress, psi Stress, psi 80000 70000 60000 50000 40000 30000 20000 10000 0 0.00 80000 70000 60000 50000 40000 30000 20000 10000 0.02 0 0.000 0.002 0.04 0.004 0.06 0.006 0.08 0.10 Strain Stress vs Strain 0.008 0.12 Elastic Modulus, E: 0.2% Offset Yield Strength, oo: Tensile Strength, ou: Breaking Strength, of: % Elongation: 0.14 0.010 0.012 0.014 Strain 0.16 0.18 0.016 0.018 0.20 0.020arrow_forwardI just can't find The percent elongation at fracture.arrow_forward
- Hello, I hope you are fine. I need to do this homework in Metal Engineering. I hope to get your help because I have an important homework.arrow_forwardA tensile test was performed on a metal specimen with a diameter of 1/2 inch and a gage length (the length over which the elongation is meas- ured) of 4 inches. The data were plotted on a load-displacement graph, P vs. AL. A best-fit line was drawn through the points, and the slope of the straight-line portion was calculated to be P/AL = 1392 kips/in. What is the modulus of elasticity? BIarrow_forwardDraw a typical stress vs strain tensile test curve for the following material and label the axis. A typical brittle material subjected to a tensile stress that has been applied to the material till the sample breaks. 1- label the axis and draw the curve for a brittle material. 2- indicate the maximum strength of the material. 3- show on the portion of the curve where young's modulus can be calculated.arrow_forward
arrow_back_ios
arrow_forward_ios
Recommended textbooks for you
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY

Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press

Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON

Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education

Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY

Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning

Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY