Lab 2 Torsion Testing
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ME 2356 Laboratory Template
1
Department of Mechanical and Industrial Engineering
ME 2356: Laboratory for Mechanics of Materials
Torsion Testing
Submitted by
Sydney Rodriguez
Date Submitted: 11/2/2023
Date Performed: 10/19/2023
Lab Section: 12
Lab TA: Lindsey Young
Course Instructor: Marguerite Matherne
ME 2356 Laboratory Template
2
1.
Introduction
The objective of this experiment was to investigate the correlation between torsional stress
and strain in various materials and to assess shear stress and strain data to determine the
shear modulus and Young's modulus
2.
Methods and results
2.1
Instron
Procedure
To conduct this experiment first the initial length and diameter of the material was
measured. Subsequently, group mates were split up to load the specimen into the Instron
machine, while the others set up the software for data collection. Finally, the test was
conducted and captured images of the fracture surface.
Results
Sample material and measurements table
Table 1. Aluminum measurements.
Parameter
Initial value
Unit
Length
66.91
mm
Diameter
6.47
mm
J
172.0351
mm
4
Torque vs. angle of twist plot
Figure 1: Torque vs. Angle of Twist plot
ME 2356 Laboratory Template
3
Stress vs. strain plot
Figure 2: Stress vs. Strain Plot
Mechanical properties table
Table 2.
Mechanical properties.
Parameter
Value
Unit
Shear modulus
2.48e+04
MPa
Yield strength
964.66
MPa
Ultimate strength
1.08e+03
MPa
Calculated elastic
modulus
6.64e+04
MPa
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ME 2356 Laboratory Template
4
Discussion
The fracture type is ductile as you can see by the photo below, the surface is smooth.
Figure 3: Fracture Surface
The calculated shear modulus was 2.48e+04 MPa, while the accepted shear modulus
for aluminum ranges from 26 to 28 GPa. Meanwhile the elastic modulus of aluminum
ranges from 69-71 GPa, which is around 3 GPa from the calculated value of 6.64e+04
MPa. Both expected values are close to the calculated values of this experiment.
Possible sources of error could be the calibration of the Isotron machine. If others
were to reconduct this experiment they would most likely gain results similar to this.
ME 2356 Laboratory Template
5
2.2
Manual tester
Procedure
During this part of the lab students were provided with the initial length and diameter of the
sample. Following this, they loaded the sample, then unloaded and reloaded it. The data was
collected and recorded in an Excel file.
Results
Sample material and measurements table
Table 3. “Brass” sample.
Parameter
Initial value
Unit
Length
80
mm
Diameter
6
mm
Torque vs. angle of twist plot
Figure 4: Torque vs. Angle of Twist Plot
ME 2356 Laboratory Template
6
Stress vs. strain plot
Figure 5: Stress vs. Strain Plot
Mechanical properties table
Table 4. Mechanical properties.
Parameter
Value
Unit
Initial shear modulus
1279
MPa
First yield strength
336
MPa
Unloading shear
modulus
1236
MPa
Second yield strength
-417
MPa
Discussion
The yield stresses calculated were .336 GPa and -.417 GPa, both values correspond
to the Bauschinger effect in which one is negative (compressive yield stress) and the
other positive (tensile yield stress).
The calculated initial shear modulus is 1.279 GPa while the expected value was 40
GPa. This could be due to improper calibration of the tester or because of a small
data sample. If this is repeated by others the data should be closer to 40 GPa.
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ME 2356 Laboratory Template
7
2.3
Poisson’s ratio
Procedure
In this procedure an axial Instron machine was operated to investigate the axial and
transverse deformation of a cork sample and a rubber band sample. Initially, the initial
dimensions were assessed, including width/diameter and height, for both samples and
photographed in their undeformed state. Subsequently, the samples were positioned
within the Instron machine, and the crank was manually manipulated to induce
deformation. Finally, images of the deformed samples were captured, and the final
width/diameter and height of each sample were measured.
Results
Sample material and measurements table
Table 5. Samples.
Parameter
Initial
Length
Initial
Width/diameter
Final
Length
Final
Width/diameter
Unit
“Rubber”
9.98
9.90
8.43
12.64
mm
“Cork”
19.92
17.18
14.40
17.33
mm
Photos of the unloaded and loaded samples
Figure 6: Unloaded Rubber Sample
ME 2356 Laboratory Template
8
Figure 7: Loaded Rubber Sample
Figure 8: Loaded Cork Sample
ME 2356 Laboratory Template
9
Figure 9: Unloaded Cork Sample
Strain
Table 5. Samples.
Parameter
Axial strain
Transverse
strain
-transverse/axial
strain ratio
“Rubber”
0.155
-0.277
0.566
“Cork”
0.277
0.00873
0.0272
Discussion
The other way of calculating Poisson’s ratio is by the following equation:
υ =
E
2G
− 1
Equation 1
In which, values for E and G, along with Poisson's ratio, can be determined using
data derived from a stress-strain diagram.
The expected value of Poisson’s ratio for rubber is 0.48-0.5 while the value for the
cork is 0. The calculated values of 0.566 for the rubber and 0.0272 for the cork are
close to the expected values. The cause of the small variation from the expected
value is most likely due to human error when taking the measurements. If repeated
other’s would likely see similar results.
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ME 2356 Laboratory Template
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Appendix:
MATLAB code
% Isotron Test
%clear data
clearvars;
clc;
%read file
filename =
'Lab2Part1.csv'
;
T = readmatrix(filename);
%sample properties (mm)
di = 6.47;
ri = di/2;
li = 66.91;
Ai = pi*(ri^2);
J = pi*(di^4)/32;
%conversions
time = T(:,2);
twist = T(:,3);
torque = T(:,4)*1000;
%stress and strain calculations
Stress = torque.*(di/(2*J))*10^3;
Strain = twist.*((di/2)*(pi/180)/li);
%plot torque vs twist
figure(1)
plot(twist, torque);
title(
'Torque vs. Angle of Twist'
);
xlabel(
'Twist (degrees)'
);
ylabel(
'Torque (Nm)'
);
hold
on
;
%plot stress vs. strain
figure(2)
plot(Strain, Stress);
title(
'Stress vs. Strain'
);
xlabel(
'Strain'
);
ylabel(
'Stress (MPa)'
);
%calculate values
ultimate_strength = max(Stress);
ultimate_torque = max(torque);
%young's modulus and shear modulus
F = polyfit (Strain (5:100), Stress(5:100),1);
E = F(1);
G = E/(2*1.34);
ME 2356 Laboratory Template
11
% Manual Tester
%clear data
clearvars;
clc;
%read file
filename =
'Lab2Part2.csv'
;
T = readmatrix(filename);
%sample properties (mm)
di = 6;
ri = di/2;
li = 80;
Ai = pi*(ri^2);
J = pi*(di^4)/32;
%conversions
twist = T(:,1);
torque = T(:,2);
%stress and strain calculations
Stress = torque.*(di/(2*J))*1000;
Strain = twist.*((di/(2*li)));
%plot torque vs twist
figure(1)
plot(twist, torque);
title(
'Torque vs. Twist'
);
xlabel(
'Twist (degrees)'
);
ylabel(
'Torque (Nm)'
);
hold
on
;
%plot stress vs. strain
figure(2)
plot(Strain, Stress);
title(
'Stress vs. Strain'
);
xlabel(
'Strain'
);
ylabel(
'Stress (MPa)'
);
%calculate values
G1 = (Stress(2)-Stress(1))/(Strain(2)-Strain(1));
G2 = (Stress(5)-Stress(6))/(Strain(5)-Strain(6));
yield1 = Stress(2);
yield2 = Stress(7);
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penetration into the barrier. (Figure 1)
Part A
P Course Home
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Determine the distance a car having a weight of 4000 lb will penetrate the barrier if it is originally traveling at 55 ft/s when it
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(D Page view
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V Draw
Problem-15-19: page-475
A 0.500-kg object attached to a spring with a force constant of 8.00 N/m vibrates in simple harmonic motion
with an amplitude of 10.0 cm. Calculate the maximum value of its
(a) speed, and acceleration.
(b) the speed and the acceleration when the object is 6.00 em from the equilibrium position, and
(c) the time interval required for the object to move from.r50 to r5 8.O0 cm.
Solution:
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Yusuf
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Engineering dynamics
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weight bearing activities.
Your boss asks you to review the technical report that was generated by the previous test engineer (whose job you now have!) and used to
verify the design. The brief report states the following... "Ti Fix-It plates were manufactured from Ti-6Al-4V (grade 5) and machined into
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plane stress representation of the point.
The state of in-plane stress at a point on an element of material is shown. Let o,
the same point that is rotated through an angle of 0-35
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In Avengers 2, Captain America's improved
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near you. Unobtainium has the normal stress-
strain diagram shown. The proportional limit,
the elastic limit and the yield point are
identical in this material.
o [MPa]
2001
175
150
125
100
Fig.1 Normal stress-strain
75
50
25
0
0. 0.05 0.1 0.15 0.2 0.25
Unobtainium has a Poisson's ratio of 0.3.
a. [6pts] Identify the yield point oy, the ultimate stress ou and the fracture
stress of. Include units.
c. [25pts] A bar of unobtainium has a length of
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mm, as shown. The cross-sectional area is
50mm 100mm = 5 x 10-³m². The bar is
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Find the normal stress in a cross-section of the bar.
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whesta fins dus al hoss
P = 375 KN
1.5 m
0.3
50 mm
100 mm
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(1)
The best least square fit parameters to the experimental data were found to be 40 mPa for the yield
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Plane-Stress Transformation
Learning Goal:
The state of in-plane stress at a point on an element of material is shown. Let |ox| = 320 MPa, |oy| = 120 MPa, and |Txy| = 75.0 MPa. Use this information to represent the state of stress of the same point that is rotated through an angle
of 0 = 25.0°.
b
Txy
σx
Part A - Normal and shear stress on element sectioned at plane a-a
Using the element sectioned at plane a-a and the rotated coordinate system shown, determine the normal and shear stresses, σ and Ta'y', respectively, acting on plane a-a.
90-0
-90-8
X
Express your answers in MPa to three significant figures separated by a comma.
0
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Ship
1,100
Model
Length (ft)
Hull Wetted Surface Area (ft2)
Speed (knots)
30
250,000
15
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70°F
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Statics of Rigid Bodies (S5)
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Content Covered:
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Statics of Rigid Bodies (S6)
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Content Covered:
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Note: Be careful with the calculations in the problem. Kindly double check the solution and answer if there is a deficiency. And also, box the final answer. Thank you so much!
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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