Torsion Testing Lab
docx
keyboard_arrow_up
School
Auburn University *
*We aren’t endorsed by this school
Course
3130
Subject
Mechanical Engineering
Date
Feb 20, 2024
Type
docx
Pages
7
Uploaded by ChancellorKoupreyPerson1035
Enoch Crittenden
eic0002@auburn.edu
February 5, 2024
Torsion Testing Lab
Objective
The objective of the lab is to determine the shear modulus of a cylindrical shaft using two methods: torsion test and torsion theory. Five loads in increments of 5 N (Newtons) are applied to the torque arm of a cylindrical copper shaft, connected
to a torsion testing machine. For each load, the strains of the three element (0-45-
90) strain gage rosettes were recorded, as well as the vertical deflection of the torque arm. This data is used to generate a Shear Stress vs. Shear Strain (
Figure 1
)
plot and a Torque vs. Angle of Twist plot and compare the shear modulus to theoretical values.
Equations
The twisting of an object due to an applied torque is torsion. The shear modulus of a material can be found through two testing methods. The first method consists of determining the applied torque and angle of twist for each load (from 5 –
25 N). The torque can be calculated:
T
=
P∙d
(
Eq. 1
)
P is the applied load and d is the length of the torque arm. To determine shear modulus using the applied torque, the angle of twist is also be solved as:
tan
θ
T
=
h
s
(
Eq. 2
)
Here, h, is the vertical deflection of the torque arm and s is the distance between the center of the shaft where h is the vertical deflection of the torque arm and s is the distance between the center of the shaft and the dial gage. The vertical deflection can be recorded from the deflection dial gage for each load. The torque and angle of twist calculated for each load were plotted against each other and a slope was found using a linear regression fit for the data using Excel. The shear modulus for this method was then found:
G
=(
T
∗
L
θ
∗
J
)
(
Eq. 3
)
G is the shear modulus, T
θ
is the slope of the plot, L is the length of the shaft, and J is the polar moment of inertia. The polar moment of inertia can be found through by the following equation:
J
=
π
∗
D
⁴
32
(
Eq. 4
)
The diameter of the shaft is denoted as D. This calculated shear modulus for method 1 can then be compared to the published shear modulus for the material to find the percent difference in the following equation:
Percent Difference
=
¿
G
−
G
th
∨
¿
G
th
∗
100
¿
(
Eq. 5
)
Another method to determine shear modulus is to find the shear stress and shear strain for each load. This can be done by a 0-45-90 strain gage rosette. Using the gage normal strains for each of the angles, the shear strain can be calculated:
γ
xy
=
2
∙Σ ε
45
−
Σ ε
0
−
Σ ε
90
(
Eq. 6
)
Shear strain (
γ
xy
) and ε
, the gage normal strain recorded for each of the three given angles. Shear stress can be calculated as:
τ
xy
=
T
∗
R
J
(
Eq. 7
)
Radius, R, is of the shaft. The shear stress and shear strain for each load are plotted against one another and linear regression is used the data to find the slope. The slope of the shear modulus and can be written as the following equation:
G
=
τ
xy
γ
xy
(
Eq. 8
)
The slope plotted is τ
xy
γ
xy
. This calculated shear modulus for method 2 can then
be compared to the published shear modulus for the material to find the difference (
Eq. 9
).
Testing
A cylindrical copper shaft was set up to a torsion testing machine. The shaft was clamped on one side and attached to a torque arm on the other. Each load was applied to the torque arm in increments of 5 N (Newtons); from 5 – 25 N. As each load is applied, the vertical deflection is recorded from the gage on the torque arm. During this process, the strain is recorded from the switch and balance unit. Both units can be changed to display the strain for each of the three angles (0-45-90). These recorded values along with the equations above were used to determine the torque, the shear strain, and angle of twist at each load. Once done, plots were then
generated, and the slope of the linear regression fit was found; this determines the shear modulus for each method. The experimental values of G are compared to the published value (G = 49000 N
mm
2
) and percent differences for both methods are calculated.
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
Results
Table 1 describes the data given corresponding to the torsion test experiment setup.
Table 2 describes the torque, shear strain, shear stress, and angle of twist.
Table 1: Measured Data
P
(N)
h
ε
0
(x 10
-6
)
ε
45
(x 10
-6
)
ε
90
(x 10
-6
)
5
0.88
-2
51
0
10
1.96
0
113
0
15
3.01
2
177
0
20
4.14
5
246
-1
25
4.47
5
265
-2
Table 2: Reduced Data
P
(N)
Torque
(T) – N*mm
Angle of Twist
(
θ
T
)
Shear Stress
(
τ
xy
)
Shear Strain
(
γ
xy
)
5
500
0.964
79.59
104
10
1000
2.146
159.20
226
15
1500
3.300
238.76
352
20
2000
4.530
318.34
488
25
2500
4.890
397.93
527
The results from Table 1 are reduced to yield the values in Table 2 by using the defined equations above. Each box was calculated and is solved as:
T
=
P ∙d
=
5
∙
100
mm
=
500
N ∙mm
– (
Eq. 1
) Torque
θ
T
=
arctan
(
h
s
)
=
arctan
(
0.88
52.3
)
=
0.964
°
– (
Eq. 2
) Angle of Twist
J
=
π D
4
32
=
π
¿¿
– (
Eq. 4
) Polar Moment of Inertia
τ
xy
=
TC
J
=
(
500
)(
4
)
25.13
=
79.59
– (
Eq. 7
) Shear Stress
γ
xy
=
(
2
∙Σ
ε
45
)
−
Σ
ε
0
−
Σ
ε
90
=
(
51
)
−
(
−
2
)
−
0
=
104
– (
Eq. 6
) Shear Strain
Using the formula to determine the percent error between the theoretical and
experimental for the Shear Modulus yields:
Percent Error
=
G
−
G
TH
G
×
100
=
49
−
47.54
49
×
100
=
¿
2.98% – (
Eq. 9
)
The shear stress values compared to the shear strain values are graphed below in Figures
(
1
), and Figure
(
2
) describes the graph between torque and angle of twist.
The shear modulus is calculated via linear regression in Excel as shown.
Figure 1: Shear Stress vs Shear Strain
Figure 2: Torque vs Angle of Twist
This lab determines the shear modulus of a material utilizing two different methods: by performing a torsion (shear) test on a shaft with a circular cross-
sectional area and application of the torsion theory. This knowledge describes how to use a torsion testing machine, read a strain indicator, use a switch, and balance unit, and properly prepare a cylindrical shaft sample with mounted three element strain rosettes. Based on the obtained percent error, the shear modulus value has
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
only a 2.98% error which means there is a minuscule error when using either method.
Related Documents
Related Questions
A high-impulse universal testing machine is being used to determine the Young's Modulus of a rectangular solid specimen (l = 20 cm, t = 1.5 cm, w = 2 cm). The machine produces 35,000 Ns that causes the impact force of compression resulted to a 1 mm deformation in the length of the specimen in 0.05 s. Determine the Young's modulus of the specimen expressed in MPa. Round off your answer to the nearest whole number
arrow_forward
5. Please calculate the strain and stress in the following two prompts
a. A 1 cm long section of tendon stretches to 1.011 cm when it is subjected to a tensile
force of 40,000 N. What is the strain in this segment of tendon?
@?
17
b. The section of the patellar ligament in the previous question is 0.02 m² in the cross
section. What is the stress in this section of ligament as a result of 50,000 N tensile
force?
E =
Δι
19
0 =
A
1.011 cm
50000
0,02
Scoco
40000
1.25
=
T
%
2500000
strain
N/m²
on trito flox your wrist, you may notice that your
arrow_forward
I need the answer as soon as possible
arrow_forward
Q-3 The following creep data were taken on an aluminum alloy at 400°C (750°F)
and a constant stress of 25 MPa (3660 psi). Plot the data as strain versus time, then
determine the steady-state or minimum creep rate.
Time
Time
(min)
Strain
(min)
Strain
0.00
18
0.82
0.22
20
0.88
4
0.34
22
0.95
0.41
24
1.03
8
0.48
26
1.12
10
0.55
28
1.22
12
0.62
30
1.36
14
0.68
32
1.53
16
0.75
34
1.77
arrow_forward
A specimen of titanium alloy is tested in torsion and the shear stress–strain diagram is shown in Fig.a. Determine the shear modulus G, the proportional limit, and the ultimate shear stress. Also, determine the maximum distance d that the top of a block of this material, shown in Fig. b, could be displaced horizontally if the material behaves elastically when acted upon by a shear force V. What is the magnitude of V necessary to cause this displacement?
arrow_forward
Part B
Data taken from a stress-strain test for a ceramic are
given in the table. The curve is linear between the origin
and the first point.
Determine the modulus of elasticity.
VO AEO vec
?
E =
ksi
Submit
Request Answer
Figure
1 of 1
Part C
σ (ksi)
e (in./in.)
Determine the modulus of resilience.
ΑΣφ
?
vec
33.2
0.0006
45.5
0.0010
in-lb
Up =
in
49.4
0.0014
51.5
0.0018
Submit
Request Answer
53.4
0.0022
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
A polypropylene has the following tensile creep compliance measured at 40
°C:
D(t) = 1.2 x t0.1 GPa-1
where t is expressed in seconds. It is subjected to the following tensile
stress sequence at 40 °C. Find the tensile strain at 3200 sec.
Stress (MPa)
1.5
1.0
0.5
1000
2000 3000
Time (s)
arrow_forward
A railroad track is laid at a temperature of 10°C with gaps of 0.008 m between the ends of the rails. The rails are 20
m long. Coefficient of thermal expansion is 11.25 x 106/°C. Modulus of elasticity = 200000 MPa. Which of the
following gives the actual deformation of the rails that will result from a temp. of 65°C?
%3D
Select one:
O a. 0.0124 m
O b. 0.0214 m
O c. 0.0142 m
O d. 0.0022 m
arrow_forward
100KN
A force of 100 KN is applied on a column as shown. The
column is made from two materials. [The top one is a
functionally graded material with a linearly varying
modulus and densities. Its length is 2 meter. The density
and elastic modulus of the top material at point A are 2700
А
kg
m3
and 72 Gpa, respectively. The density and modulus of
kg
the top material at point B are 3000 and 100 Gpa. The
m
3
В
kg
bottom material is made from steel (density =7800
and
m2
modulus=200GPA). The length of the bottom material is
1m. The cross-sections of both materials comprising the
column are cylindrical with a diameter of 0.5 m.
C
ID (oijj + bị = 0) and
considering the weight and the applied force determine:
Using equilibrium
while
The stress distribution in both members
arrow_forward
Please solve and include units in each step. Your work and solution will be appraciated much. Thank You!
arrow_forward
1. A tension test on an aluminum plate resulted in the following engineering stress-engineering strain data
as reported in the first and second column of the table below (reduction of area, RA=17%):
S (psi)
e (in/in)
σ (psi)
ε (in/in)
10500
0.001
10510.5
0.000995
21000 0.002
31200 0.003
41300 0.004
51200 0.005
61200 0.006
70600 0.007
74700 0.0075
76800 0.008
77600 0.0085
78000 0.009
78400 0.0095
78700 0.01
81200 0.02
83000 0.03
84200 0.04
85400 0.05
86200 0.06
86800 0.07
*87200 0.08
**86200 0.1
Note: *
maximum load, ** load at fracture
a) Calculate the corresponding true stress and true strain and give your results in a table along with the
engineering stress, engineering strain shown in the of table above (column 3 and 4).
b) Plot the true stress-true strain curve on a rectangular coordinate.
c) Plot the true stress-true strain curve on a log-log graph and determine the plastic flow curve parameters
K and n, the yield strength, Y, and the elastic modulus, E of the material.
arrow_forward
Determine the elastic modulus and the yield strength for the material having the stress-strain curve shown. Use the 0.2% offset method.
1600
1400
1200
E 1000
800
600
400
200
0.5
1
1.5
2
Strain, percent
Elastic modulus:
(Express your answer in whole numbers.)
E =
ksi
Yield strength:
(Express your answer using three significant figures.)
Sy =
ksi
Stress, psi
arrow_forward
You need the shear modulus for a
particular material in order to
calculate shear strain for a known
applied shear shear stress. You can't
find shear modulus for the material,
but you can find elastic modulus (200
GPa) and Poisson's ratio (0.3). Which
of the following could you use as the
shear modulus for your calculations?
200 GPa
O 60 GPa
O 77 GPa
O 154 GPa
arrow_forward
Problem 2:
A specimen of steel having an initial diameter of 0.503 in was tested in tension using a gauge length of 2
inches. The following data were obtained for the tension. Plot the stress strain data and determine the
modulus of elasticity, and the yield strength of the material.
Elastic State
Load P Ibf
Elongation in
1 000
0.0004
2 000
0.0006
3 000
0.0010
4 000
0.0013
7 000
0.0023
8 400
0.0028
8 800
0.0036
9 200
0.0089
arrow_forward
The answer is one of the options below please solve carefully and circle the correct option Please write clear .
arrow_forward
The engineering stress-strain curve below was obtained for a
precipitation hardened Aluminum alloy.
What is the approximate Yield Strength for this alloy in psi?
Engineering Stress Based on Original Area (psi)
50,000
45,000
40,000
35,000
30,000
25,000
20,000
15,000
10,000
5,000
0
O
0.02
0.04
0.06
Aluminum 6061-T6
0.08
0.1
0.12
Engineering Strain (in/in)
0.14
X
0.16
0.18
arrow_forward
You have been given the following test sample data following mechanical testing of 15
test pieces of Silicon Nitride.
What is the Weibull modulus of this material?
Would you advise the use of a similar material with a Weibull Modulus of 16.3 and a
mean failure stress of 485 MPa, if you anticipate that the peak stress on the material
could be 430 MPa?
Sample
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
Select one or more:
O a. No
O b. 18.6
O C.
13.4
O d. Yes
O e. 15.7
f. 17.1
Failure Stress (MPa)
423
459
496
432
447
467
473
499
485
479
505
530
526
490
510
<
arrow_forward
Please don't provide handwritten solution .....
arrow_forward
You have been given the following test sample data following mechanical testing of 15
test pieces of a modified Alumina.
What is the Weibull modulus of this material?
Would you advise the use of this material over one with a Weibull Modulus of 19.6 and a
mean failure stress of 270 MPa, if you anticipate that the peak stress on the material
could be 255 MPa?
Sample
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
Select one or more:
a. 185
b. No
Yes
□d. 49
□e. 28.6
3.7
Failure Stress (MPa)
297
293
270
300
g. 22.8
260
296
265
295
280
288
263
290
298
275
arrow_forward
A 11 in. inner diameter, 0.35 " wall thickness pipe is under a pressure of 2.5 ksi where strain gages installed along axial and circumferential directions register strains of 180 and 900 micro-strains (x10^-6), respectively.
A) What is the Poisson's Ratio of this material and it's Elastic Modulus?
B) In a uniaxial test, the pipe's material is observed to yield at a longitudinal strain of 0.1 in/in. Assuming a factor of safety of 2, the pipe can withstand impact energy of _______ lb - in per foot without suffering permanent deformation.
C) If the pipe is depressurized and then subjected to a torque of 50 lblb - ft.ft., it will experience a shear strain of ________ rad.
arrow_forward
A 11 in. inner diameter, 0.35 " wall thickness pipe is under a pressure of 2.5 ksi where strain gages installed along axial and circumferential directions register strains of 180 and 900 micro-strains (x10^-6), respectively.
A) What is the Poisson's Ratio of this material and it's Elastic Modulus?
B) In a uniaxial test, the pipe's material is observed to yield at a longitudinal strain of 0.1 in/in.in/in. Assuming a factor of safety of 2, the pipe can withstand impact energy of _______ lblb - in.in. per foot without suffering permanent deformation.
C) If the pipe is depressurized and then subjected to a torque of 50 lblb - ft.ft., it will experience a shear strain of ________ rad.
arrow_forward
The answer is one of the options below please solve carefully and circle the correct option Please write clear .
arrow_forward
Two composite bars have the following composition. At an initial temperature of 5 degree C, there is an existing gap of 9mm. Bar 1 and 2 have coefficiens of thermal expansion of a1=140x10^-6/°C and a2=67x10^-6/°C, respectively. Determine the temperature at which thr 9mm gap is closed.
arrow_forward
SEE MORE QUESTIONS
Recommended textbooks for you
![Text book image](https://www.bartleby.com/isbn_cover_images/9780190698614/9780190698614_smallCoverImage.gif)
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
![Text book image](https://www.bartleby.com/isbn_cover_images/9780134319650/9780134319650_smallCoverImage.gif)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
![Text book image](https://www.bartleby.com/isbn_cover_images/9781259822674/9781259822674_smallCoverImage.gif)
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
![Text book image](https://www.bartleby.com/isbn_cover_images/9781118170519/9781118170519_smallCoverImage.gif)
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
![Text book image](https://www.bartleby.com/isbn_cover_images/9781337093347/9781337093347_smallCoverImage.gif)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
![Text book image](https://www.bartleby.com/isbn_cover_images/9781118807330/9781118807330_smallCoverImage.gif)
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY
Related Questions
- A high-impulse universal testing machine is being used to determine the Young's Modulus of a rectangular solid specimen (l = 20 cm, t = 1.5 cm, w = 2 cm). The machine produces 35,000 Ns that causes the impact force of compression resulted to a 1 mm deformation in the length of the specimen in 0.05 s. Determine the Young's modulus of the specimen expressed in MPa. Round off your answer to the nearest whole numberarrow_forward5. Please calculate the strain and stress in the following two prompts a. A 1 cm long section of tendon stretches to 1.011 cm when it is subjected to a tensile force of 40,000 N. What is the strain in this segment of tendon? @? 17 b. The section of the patellar ligament in the previous question is 0.02 m² in the cross section. What is the stress in this section of ligament as a result of 50,000 N tensile force? E = Δι 19 0 = A 1.011 cm 50000 0,02 Scoco 40000 1.25 = T % 2500000 strain N/m² on trito flox your wrist, you may notice that yourarrow_forwardI need the answer as soon as possiblearrow_forward
- Q-3 The following creep data were taken on an aluminum alloy at 400°C (750°F) and a constant stress of 25 MPa (3660 psi). Plot the data as strain versus time, then determine the steady-state or minimum creep rate. Time Time (min) Strain (min) Strain 0.00 18 0.82 0.22 20 0.88 4 0.34 22 0.95 0.41 24 1.03 8 0.48 26 1.12 10 0.55 28 1.22 12 0.62 30 1.36 14 0.68 32 1.53 16 0.75 34 1.77arrow_forwardA specimen of titanium alloy is tested in torsion and the shear stress–strain diagram is shown in Fig.a. Determine the shear modulus G, the proportional limit, and the ultimate shear stress. Also, determine the maximum distance d that the top of a block of this material, shown in Fig. b, could be displaced horizontally if the material behaves elastically when acted upon by a shear force V. What is the magnitude of V necessary to cause this displacement?arrow_forwardPart B Data taken from a stress-strain test for a ceramic are given in the table. The curve is linear between the origin and the first point. Determine the modulus of elasticity. VO AEO vec ? E = ksi Submit Request Answer Figure 1 of 1 Part C σ (ksi) e (in./in.) Determine the modulus of resilience. ΑΣφ ? vec 33.2 0.0006 45.5 0.0010 in-lb Up = in 49.4 0.0014 51.5 0.0018 Submit Request Answer 53.4 0.0022arrow_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? BIarrow_forwardA polypropylene has the following tensile creep compliance measured at 40 °C: D(t) = 1.2 x t0.1 GPa-1 where t is expressed in seconds. It is subjected to the following tensile stress sequence at 40 °C. Find the tensile strain at 3200 sec. Stress (MPa) 1.5 1.0 0.5 1000 2000 3000 Time (s)arrow_forwardA railroad track is laid at a temperature of 10°C with gaps of 0.008 m between the ends of the rails. The rails are 20 m long. Coefficient of thermal expansion is 11.25 x 106/°C. Modulus of elasticity = 200000 MPa. Which of the following gives the actual deformation of the rails that will result from a temp. of 65°C? %3D Select one: O a. 0.0124 m O b. 0.0214 m O c. 0.0142 m O d. 0.0022 marrow_forward
- 100KN A force of 100 KN is applied on a column as shown. The column is made from two materials. [The top one is a functionally graded material with a linearly varying modulus and densities. Its length is 2 meter. The density and elastic modulus of the top material at point A are 2700 А kg m3 and 72 Gpa, respectively. The density and modulus of kg the top material at point B are 3000 and 100 Gpa. The m 3 В kg bottom material is made from steel (density =7800 and m2 modulus=200GPA). The length of the bottom material is 1m. The cross-sections of both materials comprising the column are cylindrical with a diameter of 0.5 m. C ID (oijj + bị = 0) and considering the weight and the applied force determine: Using equilibrium while The stress distribution in both membersarrow_forwardPlease solve and include units in each step. Your work and solution will be appraciated much. Thank You!arrow_forward1. A tension test on an aluminum plate resulted in the following engineering stress-engineering strain data as reported in the first and second column of the table below (reduction of area, RA=17%): S (psi) e (in/in) σ (psi) ε (in/in) 10500 0.001 10510.5 0.000995 21000 0.002 31200 0.003 41300 0.004 51200 0.005 61200 0.006 70600 0.007 74700 0.0075 76800 0.008 77600 0.0085 78000 0.009 78400 0.0095 78700 0.01 81200 0.02 83000 0.03 84200 0.04 85400 0.05 86200 0.06 86800 0.07 *87200 0.08 **86200 0.1 Note: * maximum load, ** load at fracture a) Calculate the corresponding true stress and true strain and give your results in a table along with the engineering stress, engineering strain shown in the of table above (column 3 and 4). b) Plot the true stress-true strain curve on a rectangular coordinate. c) Plot the true stress-true strain curve on a log-log graph and determine the plastic flow curve parameters K and n, the yield strength, Y, and the elastic modulus, E of the material.arrow_forward
arrow_back_ios
SEE MORE QUESTIONS
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
![Text book image](https://www.bartleby.com/isbn_cover_images/9780190698614/9780190698614_smallCoverImage.gif)
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
![Text book image](https://www.bartleby.com/isbn_cover_images/9780134319650/9780134319650_smallCoverImage.gif)
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
![Text book image](https://www.bartleby.com/isbn_cover_images/9781259822674/9781259822674_smallCoverImage.gif)
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
![Text book image](https://www.bartleby.com/isbn_cover_images/9781118170519/9781118170519_smallCoverImage.gif)
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
![Text book image](https://www.bartleby.com/isbn_cover_images/9781337093347/9781337093347_smallCoverImage.gif)
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
![Text book image](https://www.bartleby.com/isbn_cover_images/9781118807330/9781118807330_smallCoverImage.gif)
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY