EESHW2_Graphs
pdf
keyboard_arrow_up
School
Texas A&M University *
*We aren’t endorsed by this school
Course
320
Subject
Mechanical Engineering
Date
Feb 20, 2024
Type
Pages
3
Uploaded by DukeGalaxy9271
File:(Untitled)
3/8/2023 5:03:01 PM Page 1
EES Ver. 10.833: #2405: For use only by student and faculty in the Department of Mechanical Engineering, Texas A & M Univ
"Luke Bludau, 3/8/2023,EES HW2"
m_dot=25 [lb_m/s]
P_1=1450[psia]
T_1=850[F]
vel_2=250 [ft/s]
x_2=0.92
h_1=
enthalpy
(
Steam_IAPWS
,
T
=T_1,
P
=P_1)
h_2=
enthalpy
(
Steam_IAPWS
,
P
=P_2,
x
=x_2)
W_dot= m_dot*(h_1 - h_2)*
convert
(Btu/s, MW)
v_2=
volume
(
Steam_IAPWS
,
P
=P_2,
x
=x_2)
m_dot= vel_2*A_2/v_2
A_2= pi#
*d_2^2*
convert
(in^2,ft^2)/4
T_2=
t_sat
(
Steam_IAPWS
,
P
=P_2)
"As outlet pressure increases we see that the power output decreases negavitve exponentially. As outlet pressure increase, outlet temp increasees logirithmically. As outlet pressure increases outlet diameter decreases negative exponentially."
0
10
20
30
100
150
200
250
300
P
2
psia
T
2
[F]
Outlet Temp vs. Outlet Pressure
File:(Untitled)
3/8/2023 5:03:01 PM Page 2
EES Ver. 10.833: #2405: For use only by student and faculty in the Department of Mechanical Engineering, Texas A & M Univ
0
10
20
30
10
20
30
40
50
60
70
P
2
psia
d
2
in
Outlet Diameter vs. Outlet Pressure
File:(Untitled)
3/8/2023 5:03:01 PM Page 3
EES Ver. 10.833: #2405: For use only by student and faculty in the Department of Mechanical Engineering, Texas A & M Univ
0
10
20
30
8
8.5
9
9.5
10
P
2
psia
W
MW
Power Output vs. Outlet Pressure
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
Related Documents
Related Questions
Access Pearson
mylabmastering.pearson.com
P Pearson MyLab and Mastering
Problem 15.43
P Course Home
b Answered: HW_02.pdf EE 213-01 > Assignments HW_#...
Pearson eText
Study Area
Document Sharing
User Settings
The 20-g bullet is travelling at 400 m/s when it becomes
embedded in the 2-kg stationary block. The coefficient of
kinetic friction between the block and the plane is
μk = 0.2. (Figure 1)
Part A
Determine the distance the block will slide before it stops.
Express your answer to three significant figures and include the appropriate units.
Figure
1 of 1
με
S =
Value
Units
Submit
Request Answer
Provide Feedback
?
4 of 8
Review
Next >
arrow_forward
Part III Capstone Problem
Interactive Physics - [Lab7Part3.IP]
Eile Edit World View Object Define Measure Script Window Help
Run StoplI Reset
圖|& 品凸?
Time
Length of Spring 22
6.00
dx
Center of Mass of Rectangle 2
5.000
Tension of Rope 3
Jain@
IFI
... N
ot
rot
***lad
Split
4.000
Velocity of Center of Mass of Rectangle 2
Vx Vx
V Vy
MM
Ve
- m/s
m/s
3.00
*** m/s
Vo
..* lad/s
2 00
Center of Mass of Rectangle 1
1.000
tol
rot
*.* rad
EVelocity of Center of Mass of Rectangle 1
Vx Vx
VVy
M
0.000
-m/s
w 30
m/s
w..
MI
Ve
母100
*** m/s
Vo
... rad/s
+
EAcceleration of Center of Mass of Rectangle 1
Ax Ax
A Ay
AUJAI
Ae
--- m/s^2
... m/s^2
-- m/s^2
.-- rad/s^2
3.00
Aø
Mass M1 = 2.25 kg is at the end of a rope that is 2.00 m in length. The initial angle with
respect to the vertical is 60.0° and M1 is initially at rest. Mass M1 is released and strikes M2
= 4.50 kg exactly horizontally. The collision is elastic. After collision, mass M2 is moving on
a frictionless surface, but runs into a rough patch 2.00…
arrow_forward
5
arrow_forward
permanent-magnet (pm) genera x
Bb Blackboard Learn
L STAND-ALONE.mp4 - Google Dri x
O Google Drive: ülwgjuó jc lis u
O ME526-WindEnergy-L25-Shuja.p x
O File | C:/Users/Administrator/Desktop/KFUPM%20Term%232/ME526/ME526-WindEnergy-L25-Shuja.pdf
(D Page view
A Read aloud
T) Add text
V Draw
Y Highlight
O Erase
17
of 26
Wind Farms
Consider the arrangement of three wind turbines in the following schematic in which wind
turbine C is in the wakes of turbines A and B.
Given the following:
- Uo = 12 m/s
A
-XẠC = 500 m
-XBC = 200 m
- z = 60 m
- Zo = 0.3 m
U.
-r, = 20 m
B
- CT = 0.88
Compute the total velocity deficit, udef(C) and the velocity at wind turbine C, namely Vc.
Activate Windows
Go to Settings to activate Windows.
Wind Farms (Example Answer)
5:43 PM
A 4)) ENG
5/3/2022
I!
arrow_forward
Pearson eText
Study Area
Access Pearson
mylabmastering.pearson.com
P Pearson MyLab and Mastering
Problem 15.6
P Course Home
b Answered: HW_02.pdf EE 213-01 > Assignments HW_#...
3 of 8
■ Review
Document Sharing
User Settings
The jet plane has a mass of 250 Mg and a horizontal
velocity of 100 m/s when t = 0.
Part A
If both engines provide a horizontal thrust which varies as shown in the graph in (Figure 1), determine the plane's velocity in 5 s.
Neglect air resistance and the loss of fuel during the motion.
Express your answer to three significant figures and include the appropriate units.
Figure
1 of 1
>
☐
μÅ
?
v =
Value
Units
Submit
Request Answer
Provide Feedback
Next >
arrow_forward
(b): Let us first consider controlling the orbit of deputy spacecraft to rendezvous with chief spacecraft.
Define x = [r] and x = x = R to represent the deputy orbital state and its target (= chief
orbit) in Cartesian coordinates, respectively. The control input is thruster acceleration, u € R³, in the
ECI frame. Denote the relative state by dx = x-x. Table 2 summarize the initial orbital elements.
Table 2: Keplerian orbital elements at epoch (t = 0) for deputy and chief about Earth (ECI frame)
Orbital element
Deputy
Unit
Chief
semi-major axis
ad =
11500
ac 10000 km
eccentricity
inclination
ed = 0.15
id=35
ee = 0.3
i = 50
degree
right ascension of ascending node d = 50
Ως = 50
degree
argument of periapsis
true anomaly at epoch
Wd
Vd= 0
=
40
We =
40
degree
Ve=0
degree
(b.1): Derive the error dynamics of our system in ECI frame under the influence of u.
(b.2): Consider a candidate Lyapunov function V = ½dr¹ K₁dr+dv₁dv, where K₁ = K, and K, > 0.
Discuss the positive definiteness of V, and…
arrow_forward
汇
Advertised missile performance:
Natural Frequency 0.65
a = Angle of attack [rad]
q = pitch rate [rad]
= 1.25m center of gravity
Xcg
Zcg = Om center of gravity
The equations of motion for the missile are
a = q - 0.435sin a + 0.07a -0.00014q
q = 111.484(xcg - 1.483)a - (2.2968 - 3.156zcg)q +3.448 + 137895Zcg
To acquire the target the missile needs to fly at
α = 0.017 [rad] qo= 0 [rad/s] = 0 [rad]
So
Determine if the missile is stable about the given equilibrium point.
arrow_forward
21/Prove
Cr =
(
Tmax)
Tmin
2(8-1)
22/ derivation of equation
Wnet
=
?
Cv [T3-T₂] - Cv [T₁ - T₁ ] ?
arrow_forward
HW_5_01P.pdf
PDF
File | C:/Users/Esther/Downloads/HW_5_01P.pdf
2 Would you like to set Microsoft Edge as your default browser?
Set as default
To be most productive with Microsoft Edge, finish setting up your
Complete setup
Maybe later
browser.
(D Page view A Read aloud V Draw
7 Highlight
2
of 3
Erase
5. Two cables are tied to the 2.0 kg ball shown below. The ball revolves in a horizontal
circle at constant speed. (Hint: You will need to use some geometry and properties of
triangles and their angles!)
60°
1.0 m
60°
© 2013 Pearson Education, Inc.
(a) For what speed is the tension the same in both cables?
(b) What is the tension?
2.
2:04 PM
O Type here to search
C A
2/9/2021
(8)
arrow_forward
Study Area
Document Sharing
User Settings
Access Pearson
mylabmastering.pearson.com
P Pearson MyLab and Mastering
The crash cushion for a highway barrier consists of a
nest of barrels filled with an impact-absorbing material.
The barrier stopping force is measured versus the vehicle
penetration into the barrier. (Figure 1)
Part A
P Course Home
b My Questions | bartleby
Review
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
strikes the first barrel.
Express your answer to three significant figures and include the appropriate units.
Figure
1 of 1
36
μΑ
S =
Value
Units
Submit
Request Answer
Provide Feedback
?
Next >
arrow_forward
хоос»
0 Python 3 (p
Define a python function to determine the 2nd moment of area I, under the parabola, with respect to the centroidal-axis. The
parabolic curve is defined as z = ky2, where k = b/h². The centroidal axis has a given distance d with respect to z axis.
Hints: Use the parallel axis theorem. Find the 2nd moment of area against z axis first and then use the formula I₂ = I₁ + d²A to
calculate I, where d is a given value (no need to derive). Note that this question requires you to derive the equation first.
$
4
l) | Idle Mem: 260.77/12288.00 MB
Q
F4
R
y
1
1
0
do 5
[ ]: # Complete the function given the variables b,h,d and return the value as "Area","Iz" and "Ic"
# This is not about numerical integration, we only need the analytical solution.
# Don't change the predefined content, only fill your code in the region "YOUR CODE"
Mode: Command
%
9
F5
0
T
.
Markdown v
z = ky²
2
6
C
F6
Validate
Y
&
7
8:
F7
U
*
8
DII
F8
I
19
F9
b
O
)
Ln 1, Col 1 English (United States)…
arrow_forward
For the given Two Link Manipulator (Fig 1),
If 11-1m and 12=1m
01-40° and 02-10°
Calculate the coordinates of the end effector (x,y)
arrow_forward
13. User tool frame UT[3] was set up by the programmer with three-point method for UT setup
provided by FANỤC robot system. Which of the following statements is correct.
(a) UT[3] frame is measured relative to UF[h] frame.
(b) The orientation of UT[3] frame is the same as the orientation of default TCP frame (i.e. Def-
TCP frame).
(c) The origin of UT[3] frame is exactly aligned to the origin of default Def-TCP frame.
14. Using three-point method for user tool frame UT[k] setup, a robot programmer can set up the user-
defined
of UT[k] for an end-effector.
(a) position (i.e. origin)
(b) orientation
(c) position (i.e. origin) and orientation
arrow_forward
Draw the operating curves of the given system on the graph using all necessary curves in excel
ÖN = 5 so you must choose the correct H equation
arrow_forward
Page 8/5
Q4: (M4)
LE
Velocity: V [km/hr]
Wavelength: L [m]
M
k
y(t)
Model
Height: H [m]
The figure above shows a model of a person riding a unicycle that contains a spring
under its seat. The spring constant is k = 10,600 N/m. Assume that damping is minimal,
the wheel of the unicycle has no mass and is not a spring, the unicyle always stays
perfectly upright, and the person is represented by a rigid mass M = kg.
a) When the unicycle is being ridden at speed V = 10 km/hr over the sinusoidal bumpy
terrain shown above, with bump spacing L=0.6 m and bump height H 0.05 m, what
will be the steady-state peak-to-peak amplitude of the motion y(t) [m] of the person
riding the unicycle?
b) Recalculate the steady-state peak-to-peak amplitude of the motion for 2.5, 5, and 20
km/hr. Will the rider have difficulty reaching speeds above 5 km/hr?
arrow_forward
create matlab code and screen shot both files
arrow_forward
T
FL
%24
E
Tradi
G 0.169 iGen selec +
Launc
- SIS S
25 (25) V
Teleg
3 Drop
do,
-bf M Inbc
heducation.com/ext/map/index.html?_con%3Dcon&lexternal_browser%3D0&launchUrl=https%253A%252F%252Fnewconnect.mheducation.com%252F#/activity/c
Help
Save &
Saved
Required information
A cylindriçal fuel rod (k 30 W/m K) of 2 cm in diameter is encased in a concentric tube and cooled by water. The fuel rod
generates heat uniformly at a rate of 100 MW/m, and the average temperature of the cooling water is 80°C with a
convection heat transfer coefficient of 2500 W/m4-K. The operating pressure of the cooling water is such that the surface
temperature pf the fuel rod must be kept below 200°C to avoid the cooling water from reaching the critical heat flux (CHF).
The crițical heat flux is a thermal limit at which a boiling crisis can occur that cause overheating on the fuel rod surface and
lead to damage.
ė ren = 100 MW/m3
%3D
Cooling water
Fuel rod
D=2 cm
2500 W/m2-K
Determine the temperature of the fuel rod…
arrow_forward
E Machine Design & CAD-II (Engr. x
O Shigley's Mechanical Engineering X
+
O File
C:/SEMMESTER%2306/Machine%20Design%20and%20CAD/Shigley's%20Mechanical%20Engineering%20Design,%2010th%20Edition.pdf
Shigley's Mechanical Engineering Design, Tenth Edition
737 / 1105
200%
+
3-17
Shaft a in the figure rotates at 600 rev/min in the direction shown. Find the speed and direction
of rotation of shaft d.
207, = 30° RH
736
8T, = 60° RH
13-17
3
737
40T
177, = 30° RH
20T
60T
Shigley's Mechanic.pdf
Show all
W
7:22 PM
5/16/2021
II
国
arrow_forward
mylabmastering.pearson.com
Chapter 12 - Lecture Notes.pptx: (MAE 272-01) (SP25) DY...
P Pearson MyLab and Mastering
Scores
arrow_forward
Motiyo
Add explanation
arrow_forward
21. The programmer uses three-point method for UT[2] setup for a sharp-tip pointer. If the
programmer recorded each of three-points by precisely contacting the sharp-tip to the tip of the
stationary reference pointer on the table, then
(a) UT[2] setup is accurate
(b) UT[2] setup is not accurate
(c) the accuracy of UT[2] setup is still uncertain
22. User frame UF[3] is accurately set up on the part reference surface which is unparallel to the
surface where the robot is mounted. To jog the robot TCP to move perpendicularly to the part
reference surface, the programmer
(a) needs to select World jogging coordinate system
(b) needs to activate UF[3] and select User Frame jogging coordinate system
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
- Access Pearson mylabmastering.pearson.com P Pearson MyLab and Mastering Problem 15.43 P Course Home b Answered: HW_02.pdf EE 213-01 > Assignments HW_#... Pearson eText Study Area Document Sharing User Settings The 20-g bullet is travelling at 400 m/s when it becomes embedded in the 2-kg stationary block. The coefficient of kinetic friction between the block and the plane is μk = 0.2. (Figure 1) Part A Determine the distance the block will slide before it stops. Express your answer to three significant figures and include the appropriate units. Figure 1 of 1 με S = Value Units Submit Request Answer Provide Feedback ? 4 of 8 Review Next >arrow_forwardPart III Capstone Problem Interactive Physics - [Lab7Part3.IP] Eile Edit World View Object Define Measure Script Window Help Run StoplI Reset 圖|& 品凸? Time Length of Spring 22 6.00 dx Center of Mass of Rectangle 2 5.000 Tension of Rope 3 Jain@ IFI ... N ot rot ***lad Split 4.000 Velocity of Center of Mass of Rectangle 2 Vx Vx V Vy MM Ve - m/s m/s 3.00 *** m/s Vo ..* lad/s 2 00 Center of Mass of Rectangle 1 1.000 tol rot *.* rad EVelocity of Center of Mass of Rectangle 1 Vx Vx VVy M 0.000 -m/s w 30 m/s w.. MI Ve 母100 *** m/s Vo ... rad/s + EAcceleration of Center of Mass of Rectangle 1 Ax Ax A Ay AUJAI Ae --- m/s^2 ... m/s^2 -- m/s^2 .-- rad/s^2 3.00 Aø Mass M1 = 2.25 kg is at the end of a rope that is 2.00 m in length. The initial angle with respect to the vertical is 60.0° and M1 is initially at rest. Mass M1 is released and strikes M2 = 4.50 kg exactly horizontally. The collision is elastic. After collision, mass M2 is moving on a frictionless surface, but runs into a rough patch 2.00…arrow_forward5arrow_forward
- permanent-magnet (pm) genera x Bb Blackboard Learn L STAND-ALONE.mp4 - Google Dri x O Google Drive: ülwgjuó jc lis u O ME526-WindEnergy-L25-Shuja.p x O File | C:/Users/Administrator/Desktop/KFUPM%20Term%232/ME526/ME526-WindEnergy-L25-Shuja.pdf (D Page view A Read aloud T) Add text V Draw Y Highlight O Erase 17 of 26 Wind Farms Consider the arrangement of three wind turbines in the following schematic in which wind turbine C is in the wakes of turbines A and B. Given the following: - Uo = 12 m/s A -XẠC = 500 m -XBC = 200 m - z = 60 m - Zo = 0.3 m U. -r, = 20 m B - CT = 0.88 Compute the total velocity deficit, udef(C) and the velocity at wind turbine C, namely Vc. Activate Windows Go to Settings to activate Windows. Wind Farms (Example Answer) 5:43 PM A 4)) ENG 5/3/2022 I!arrow_forwardPearson eText Study Area Access Pearson mylabmastering.pearson.com P Pearson MyLab and Mastering Problem 15.6 P Course Home b Answered: HW_02.pdf EE 213-01 > Assignments HW_#... 3 of 8 ■ Review Document Sharing User Settings The jet plane has a mass of 250 Mg and a horizontal velocity of 100 m/s when t = 0. Part A If both engines provide a horizontal thrust which varies as shown in the graph in (Figure 1), determine the plane's velocity in 5 s. Neglect air resistance and the loss of fuel during the motion. Express your answer to three significant figures and include the appropriate units. Figure 1 of 1 > ☐ μÅ ? v = Value Units Submit Request Answer Provide Feedback Next >arrow_forward(b): Let us first consider controlling the orbit of deputy spacecraft to rendezvous with chief spacecraft. Define x = [r] and x = x = R to represent the deputy orbital state and its target (= chief orbit) in Cartesian coordinates, respectively. The control input is thruster acceleration, u € R³, in the ECI frame. Denote the relative state by dx = x-x. Table 2 summarize the initial orbital elements. Table 2: Keplerian orbital elements at epoch (t = 0) for deputy and chief about Earth (ECI frame) Orbital element Deputy Unit Chief semi-major axis ad = 11500 ac 10000 km eccentricity inclination ed = 0.15 id=35 ee = 0.3 i = 50 degree right ascension of ascending node d = 50 Ως = 50 degree argument of periapsis true anomaly at epoch Wd Vd= 0 = 40 We = 40 degree Ve=0 degree (b.1): Derive the error dynamics of our system in ECI frame under the influence of u. (b.2): Consider a candidate Lyapunov function V = ½dr¹ K₁dr+dv₁dv, where K₁ = K, and K, > 0. Discuss the positive definiteness of V, and…arrow_forward
- 汇 Advertised missile performance: Natural Frequency 0.65 a = Angle of attack [rad] q = pitch rate [rad] = 1.25m center of gravity Xcg Zcg = Om center of gravity The equations of motion for the missile are a = q - 0.435sin a + 0.07a -0.00014q q = 111.484(xcg - 1.483)a - (2.2968 - 3.156zcg)q +3.448 + 137895Zcg To acquire the target the missile needs to fly at α = 0.017 [rad] qo= 0 [rad/s] = 0 [rad] So Determine if the missile is stable about the given equilibrium point.arrow_forward21/Prove Cr = ( Tmax) Tmin 2(8-1) 22/ derivation of equation Wnet = ? Cv [T3-T₂] - Cv [T₁ - T₁ ] ?arrow_forwardHW_5_01P.pdf PDF File | C:/Users/Esther/Downloads/HW_5_01P.pdf 2 Would you like to set Microsoft Edge as your default browser? Set as default To be most productive with Microsoft Edge, finish setting up your Complete setup Maybe later browser. (D Page view A Read aloud V Draw 7 Highlight 2 of 3 Erase 5. Two cables are tied to the 2.0 kg ball shown below. The ball revolves in a horizontal circle at constant speed. (Hint: You will need to use some geometry and properties of triangles and their angles!) 60° 1.0 m 60° © 2013 Pearson Education, Inc. (a) For what speed is the tension the same in both cables? (b) What is the tension? 2. 2:04 PM O Type here to search C A 2/9/2021 (8)arrow_forward
- Study Area Document Sharing User Settings Access Pearson mylabmastering.pearson.com P Pearson MyLab and Mastering The crash cushion for a highway barrier consists of a nest of barrels filled with an impact-absorbing material. The barrier stopping force is measured versus the vehicle penetration into the barrier. (Figure 1) Part A P Course Home b My Questions | bartleby Review 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 strikes the first barrel. Express your answer to three significant figures and include the appropriate units. Figure 1 of 1 36 μΑ S = Value Units Submit Request Answer Provide Feedback ? Next >arrow_forwardхоос» 0 Python 3 (p Define a python function to determine the 2nd moment of area I, under the parabola, with respect to the centroidal-axis. The parabolic curve is defined as z = ky2, where k = b/h². The centroidal axis has a given distance d with respect to z axis. Hints: Use the parallel axis theorem. Find the 2nd moment of area against z axis first and then use the formula I₂ = I₁ + d²A to calculate I, where d is a given value (no need to derive). Note that this question requires you to derive the equation first. $ 4 l) | Idle Mem: 260.77/12288.00 MB Q F4 R y 1 1 0 do 5 [ ]: # Complete the function given the variables b,h,d and return the value as "Area","Iz" and "Ic" # This is not about numerical integration, we only need the analytical solution. # Don't change the predefined content, only fill your code in the region "YOUR CODE" Mode: Command % 9 F5 0 T . Markdown v z = ky² 2 6 C F6 Validate Y & 7 8: F7 U * 8 DII F8 I 19 F9 b O ) Ln 1, Col 1 English (United States)…arrow_forwardFor the given Two Link Manipulator (Fig 1), If 11-1m and 12=1m 01-40° and 02-10° Calculate the coordinates of the end effector (x,y)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

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