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Tensile Test Experiment
ME 3228: Materials and Mechanics Lab
Section: 519
Tyler Myers
Due: March 6
th
Turn in to: Cargi M, Bakirci
Summary
For the Tensile Test Experiment, data was collected from using an MTS machine
and lab computer. The data collected was the position and load of what was going on
to a sample material. The materials used were two different types of aluminum and
steel. The simple tensile test was performed on each of the four samples. With the
data found in the experiment, calculations of stress and strain were done, finding the
different material properties of the four samples. With the stress and strain values,
graphs were created to illustrate the experiment, and with those graphs some of the
material properties were directly found. The material properties consisted of
elasticity, yield and ultimate strengths, resilience, toughness, percentage of
elongation, and percentage of reduction in area of the samples. As for most of the
material properties, having to have been calculated, charts were drawn up for the
comparison of the experimental data to the real world reference data provided by any
common engineering book. Details of the experiment and its results will be provided
later in the report, along with all the tables and graphs generated from the
experiment’s data.
- List of Figures ________________________________________________________
- List of Tables ________________________________________________________
- List of Equations ________________________________________________________
- Summary ________________________________________________________
- Introduction ________________________________________________________
- Theory ________________________________________________________
- Test Description ________________________________________________________
- Results ________________________________________________________
- Discussion ________________________________________________________
- Conclusion ________________________________________________________
- References ________________________________________________________
- Appendix ________________________________________________________
- Figure 1: Tensile Test in Action List of Figures
- Figure 2: The MTS Machine
- Figure 3: Four Different Sample Materials
- Figure 4: The Stress-Strain Graph of ASIS
- Figure 5: The Stress-Strain Graph of AISI
- Figure 6: The Stress-Strain Graph of Al
- Figure 7: The Stress-Strain Graph of Al
- Figure 8: The .2% Offset Graph of AISI
- Figure 9: The .2% Offset Graph of AISI
- Figure 10: The .2% Offset Graph of Al
- Figure 11: The .2% Offset Graph of Al
- Figure 12: The Young’s Modulus Graph of AISI
- Figure 13: The Young’s Modulus Graph of AISI
- Figure 14: The Young’s Modulus Graph of AL
- Figure 15: The Young’s Modulus Graph of Al
- Figure 16: The Elasticity Comparison Chart
- Figure 17: The Yield Strength Comparison Chart
- Figure 18: The Ultimate Strength Comparison Chart
- Figure 19: The Comparison between Ductile and Brittle Fractures
List of Tables
Table 1: Initial and Final Measurements of the Sampled Material 11
Table 2: Experimental Mechanical Properties of Four Samples 23
Table 3: The Comparison Table between the Experimental and Referenced Data 23
Introduction
This experiment consisted of measuring the mechanical properties of two
different types of materials using a tensile testing machine. The purpose of this
experiment is to recreate a real world application of what these materials might be
subjected to when the materials are put to work. These experiments are done often
to construct a set of data for all engineers to be able to have quick access to correct
information and material specifications and properties. So with this type of
experiment, the elastic modulus, the ultimate strength, and the yield strength can be
calculated and compared to old references from previous experiments to see how the
material properties have changed, if any. The two materials being tested in this
experiment will be steel and aluminum. Those two types of materials have also been
split into two sub-types: Steel: 1018 and 1045, Al: 7075 and 6061.
Theory
The idea of this tensile test experiment is to calculate the specific material
properties from each material tested and see how they compare to a standard
reference of the same material’s properties already provided in the real world. Below
is a snap shot of an actual tensile test being taken on a sample material.
Figure 1: Tensile Test in Action
The specific properties the experiment will provide will be elasticity, yield and
ultimate strengths, resilience, toughness, percentage of elongation, and percentage
of reduction in area of the samples. Finding these will have to come from finding the
tensile stress of the experiment being performed. The tensile stress, σ, is calculated
through this equation:
𝐴𝑜^ (Equ. 1)
Where F is the load being applied and A 0 is the original cross-sectional area at the gage
section of the sample. Then the strain, ε, is also needed for calculations purposes to
measure what is being done to the sample in terms of it being stretched out. The
engineering strain is calculated by:
𝑙 0 (Equ. 2)
Here, l is the new gage length and l 0 is the original gage length. With the calculations
of both the stress and strain of the sample, a Stress vs. Strain graph can then be created
to see how the sample acts while the tensile test is being performed. After setting up
a proper stress-strain graph, the calculation of the modulus of elasticity, E, can be
found using the simple slope definition:
∆𝜀 (Equ. 3)
With the elasticity, obtaining the yield strength is done by performing a .2% offset on
the stress-strain graph, and figuring out where the two lines intersect. The Ultimate
tensile strength, σu, is found by:
𝜎𝑢 = 𝐹𝑚/𝐴 0 (Equ. 4)
With Fm being the maximum load applied to the sample. Resilience, or the energy
absorbed by the sample when it is being deformed elastically, is found by using:
2 𝜎𝑦^ ∗ 𝜀𝑦^ (Equ. 5)
Figure 2: The MTS Machine
The samples being tested in this experiment are AISI 1018, AISI 1045, Aluminum 6061-
T6, Aluminum 7075-T24.
Figure 3: Four Different Sample Materials
During the Tensile Test experiment, the four samples were measured for their original
gage length and diameters. Each sample was then put in and clamped down by the
upper and lower hydraulic grips. Then using the lab computer, the MTS machine was
activated, calibrated, and began pulling the sample down with the lower grip while the
upper grip remained stationary. During this, the computer stores the data of the
position of the grips, and the load that is being applied to the sample at the current
time. The sample was then pulled until fracture. Once fracture was reached, the
machine was deactivated. The sample was then measured once more for its final gage
length and diameters.
Results
The first thing in this experiment was to document the initial gage length and
diameters of the sample, immediately following fracture of the sample, the final gage
length and diameters were taken.
Table 1: Initial and Final Measurements of the Sampled Material
Sample
Gage Diameter Gage Length Cross-Sectional
(cm) (cm) Area (cm)
Initial Final Initial Final Initial Final
After the experiment, calculations to find the stress and strain were done on each
sample. With those stress and strain values, a Stress-Strain graph was created per
sample. Shown next are the four samples Stress-Strain graphs.
Figure 6: The Stress-Strain Graph of Al 6061
Figure 7: The Stress-Strain Graph of Al 7075
Stress (MPa)
Strain
Stress vs Strain Graph, 6061
Exp. Data
Stress (MPa)
Strain
Stress vs Strain Graph, 7075
Exp. Data
With the Stress-Strain graphs generated per sample, a .2% Offset graph was created to
find the values of the yield strength of the samples.
Figure 8: The .2% Offset Graph of AISI 1018
Figure 9: The .2% Offset Graph of AISI 1045
Stress (MPa)
Stain
.2% Offset Graph, 1018
Exp. Data .2% offest
Stress (MPa)
Strain
.2 % Offset Graph, 1045
Exp. Data .2% Offset
To do so, a simple calculation of Young’s Modulus had to be done in order to find, E,
the elasticity of the sample to create the .2% Offset Graph. The Young’s Modulus was
calculated by finding the slope of the original data of stress and strain using up to the
first one hundred to two hundred megapascals of stress for ease of finding the
equation of the line. The following four graphs illustrate the linear relationship of the
Young’s Modulus for the samples.
Figure 12: The Young’s Modulus Graph of AISI 1018
Stress (MPa)
Strain
Young's Modulus Graph, 1018
Exp. Data Linear (Exp. Data)
Figure 13: The Young’s Modulus Graph of AISI 1045
Figure 14: The Young’s Modulus Graph of AL 6061
Stress (MPa)
Strain
Young's Modulus Graph, 1045
Exp. Data Linear (Exp. Data)
Stress (MPa)
Strain
Young's Modulus Graph, 6061
Exp. Data Linear (Exp. Data)
Figure 16: The Elasticity Comparison Chart
Next is the comparison of the Yield strengths for the four samples.
Figure 17: The Yield Strength Comparison Chart
Elasticity (GPa)
Exp. Ref.
Yield Strength (MPa)
Exp. Ref.
Lastly, illustrated below is the comparison of the Ultimate Strengths of the four
samples.
Figure 18: The Ultimate Strength Comparison Chart
Discussion
There appears to be a clear difference between the two steel and the two
aluminum materials upon completion of the results for the experiment. When talking
about the two steel materials, AISI 1045 shows a clear difference in its ability to hold a
greater force when compared to the AISI 1018. Its ultimate strength is greater, but its
yield strength is lower. AISI 1045 also has a greater elasticity, meaning it is less brittle.
When comparing the two aluminum materials, the Al 7075’s yield and ultimate
strengths are higher than the Al 6061. But the elasticity of the Al 6061 is greater than
the Al 7075 as far as the experimental data, but in a perfect analysis, the Al 7075 should
have a greater elasticity, meaning that the Al 6061 is less ductile than the Al 7075.
Looking at the aluminum and steel materials together, even from the tensile test
experimental data, the steel’s properties of elasticity, yield and ultimate strengths are
far beyond those of the aluminums. Which makes sense knowing that the steel should
be far more brittle and the aluminum more ductile. With being more brittle, the steel
Ultimate Strength (Mpa)
Exp. Ref.