SlideShare a Scribd company logo
1 of 17
Download to read offline
CEE170: Introduction to Fluid Mechanics
Water Jet Cart Design Project

Group 18: Top Crew
Chosita Sribhibhadh
Kevin Krik
Patricia Kharazmi
Megan Hanrahan
Saman Shaolian
Ali Behbahani
Toni Lynch

1
Table of Contents
Section Title

Page Number

Introduction…………………………………………………………… 3
Predicting the Velocity of the Water Jet………..…………………….. 3
Predicting the Rate of Change of Tank Water Height over Time….…. 6
Predicting the Speed of the Cart............................................................. 7
Predicting the Distance the Cart Will Travel…….…………………… 8
The Matlab Code……………………………………………………… 8
Tank Options and Specifications……………………………..……...... 9
Cart Materials and Design……………....…………………………..... 10
Preliminary Cart Testing Results…………………………….……….. 11
Final Cart Race Results……………………………………………….. 12
Race Videos and Pictures.…………………………………………….. 13
Appendix…………………………………………………………….… 14
Resources……………………………………………………………… 17

2
Introduction
The purpose of this project is to design a cart that can travel a 50 foot distance along a 2% slope
with a high speed. Each group should be able to predict the speed of their cart based on Matlab
modeling and calibration of these models due to preliminary testing. The goal of the project is to
design a cart with the fastest design speed or have the closest prediction of time using the test
data and Matlab model. Provided is a pressurized tank filled with water. The tank has a nozzle of
interchangeable diameter that will shoot out a jet of water. The teams’ job is to design a chamber
to attach to the cart that will catch the water jet and use it to propel the cart forward and to
choose certain tank specifications that will lead to a successful run.

Predicting the Velocity of the Water Jet
The energy equation, which comes from conservation of energy in the Reynolds Transport
Theorem is used to find the velocity of the water jet. Here is how the equation used is derived:
Sketch of pressurized tank:

2
𝑃1
𝑉12
𝑃2
𝑉2
+
+ 𝑍1 + ℎ 𝑝 =
+
+ 𝑍2 + ℎ 𝑡 + ℎ 𝐿
𝛾 2𝑔
𝛾 2𝑔

3












P1 is the pressure in the tank, which can be denoted as P
γ is the density of water (ρ=998 kg/m3) multiplied by the acceleration of gravity (g=9.81
m/s2)
V1 is the velocity of the water in the tank, which is such a small number, it can be
considered zero
Z1 is the height of water in the tank
P2 is the pressure at point 2 and since it is open to the atmosphere, it can also be consider
zero
V2 is the velocity of the water jet which can be denoted as VJ
Z2 is the height of the centerline of the nozzle
hp is the height of energy gained due to a pump, but since there is no pump, it equals zero
ht is the height of energy removed from the system by a turbine, this term also equals
zero
hL is the height of energy lost due to friction in the nozzle
A new variable h is used to represent the height of the water in the tank to the centerline
of the nozzle where: ℎ = 𝑍1 − 𝑍2

Taking all these factors into account, the equation is then simplified to:

𝑉𝐽2
𝑃
+ℎ =
+ℎ𝐿
𝛾
2𝑔
𝐿

where ℎ 𝐿 = (𝐾𝑣 + 𝑓 )

2
𝑉𝐽

𝑑 2𝑔






Kv is the minor loss coefficient
𝑓 is the friction factor
L is the length of the nozzle
d is the diameter of the nozzle

The simplified energy equation now becomes:

𝑉𝐽2
𝑃
𝐿
+ℎ=
(1 + 𝐾 + 𝑓 )
𝛾
2𝑔
𝑑
Finally, solving for VJ results in the equation:

𝑃
2𝑔 ( 𝛾 + ℎ)
𝑉𝐽 = √
𝐿
1+ 𝐾+ 𝑓
𝑑

4
The equation that accounts for the change in pressure in the tank over time is:
𝑘
𝑠
)
𝑃 = 𝑃0 (
𝑠 + ℎ0 + ℎ





P0 is initial pressure in the tank
s is the initial height from the top of the tank to the water in the tank
h0 is the initial height of water in the tank
 k is the ratio of specific heats inside and outside of the tank
This equation must be plugged into the equation for VJ for accuracy:
𝑘
𝑠
)
𝑃0 (
𝑠 + ℎ0 + ℎ
2𝑔 (
+ ℎ)
𝛾

𝑉𝐽 =
√

1+ 𝐾+ 𝑓

𝐿
𝑑

5
Predicting the Rate of Change of Tank Water Height over Time
Now that the velocity of the water jet has been estimated, it can be used to estimate the rate at
which the height of the water in the tank changes over time. The volume of water changing in the
tank over time can be expressed as:

𝑑𝑉 𝑡𝑎𝑛𝑘
= −𝑄 𝑜𝑢𝑡
𝑑𝑡


Qout is the flow of water out of the tank (A2V2) which can be written as:

𝑄 𝑜𝑢𝑡 =

𝜋 2
𝑑 𝑉𝐽
4

Since the diameter of the tank always remains constant, the expression for the change in volume
of the tank can be written as:

𝑑𝑉 𝑡𝑎𝑛𝑘
𝜋
𝑑ℎ
= 𝐷2
𝑑𝑡
4
𝑑𝑡


D is the diameter of the tank
 dh/dt is the change in height of the water over time
Substituting these two equations into the original results in:

𝜋 2 𝑑ℎ
𝜋
𝐷
= − 𝑑 2 𝑉𝐽
4
𝑑𝑡
4
Solving for dh/dt gives:

𝑑ℎ
𝑑2
= (− 2 𝑉𝐽 )
𝑑𝑡
𝐷
Plugging the jet velocity equation into this equation supplies the first ordinary differential
equation (ODE) that will be solved in Matlab:
𝑘
𝑠𝑜
2∗(𝑔∗ℎ+(𝑃𝑜∗( 𝑠𝑜+ℎ𝑜−ℎ) ))

(
𝑑ℎ
𝑑2
=− 2∗
𝑑𝑡
𝐷

𝑝

0.5

)

𝐿
1 + 𝐾𝑣 + 𝑓 ∗ ( )
𝑑
(

)

6
Predicting the Speed of the Cart
Once the velocity of the water jet has been predicted, that value, along with the dimensions of
the cart design can be used to predict the speed of the cart. The prediction of the cart’s speed
comes from Newton’s Second Law of Motion Equation (Σ𝐹 = 𝑚𝑎). Accounting for all the
forces acting on the cart gives the equation:

𝐹𝐽 − 𝐹 𝐺 − 𝐹 𝑅 = 𝑚𝑎
Solving the equation for acceleration gives:

𝑎=


𝐹𝐽 − 𝐹 𝐺 − 𝐹 𝑅
𝑚

FJ is the force exerted on the cart by the jet, which can be written as:

𝐹𝐽 = 𝛼𝜌𝐴 𝐽 𝑉 2
𝑅
o α is the momentum transfer coefficient (calibration parameter from 0-2)
o AJ is the area of the water jet (π/4*d2)
o VR is the relative velocity between the jet and the cart (V J-VC)


FG is the gravitational force on the cart which can be written as:

𝐹 𝐺 = 𝑚𝑔𝑠𝑖𝑛𝜃
o θ is the angle of incline
o m is the mass of the cart


FR is the force due to rolling friction and air resistance which can be ignored in further
calculations

Plugging all of these forces into Newton’s Equation solved for acceleration gives:

𝛼𝜌𝐴 𝐽 𝑉 2
𝑅
𝑎=
− 𝑔𝑠𝑖𝑛𝜃
𝑚
Knowing that acceleration is the change in velocity over time (𝑎 =
rewritten as:

𝑑𝑉 𝑐
𝑑𝑡

), this equation can be

𝛼𝜌𝐴 𝐽 𝑉 2
𝑑𝑉 𝐶
𝑅
=
− 𝑔𝑠𝑖𝑛𝜃
𝑑𝑡
𝑚
Accounting for deceleration due to drag and friction (Cdf) supplies the second ODE to be solved
in Matlab:

𝛼𝜌𝐴 𝐽 𝑉 2
𝑑𝑉 𝐶
𝑅
=
− 𝑔𝑠𝑖𝑛𝜃 − 𝐶 𝑑𝑓
𝑑𝑡
𝑚

7
Predicting the Distance the Cart Will Travel
Now that the speed of the cart has been predicted, the distance it will travel can also be predicted.
The total distance the cart will travel is simply the change in the cart’s velocity over time. This
can be expressed as:

𝑑𝑥 = 𝑉𝑐 𝑑𝑡
Solving for velocity supplies the third ODE to be solved in Matlab:

𝑑𝑥
= 𝑉𝑐
𝑑𝑡

The Matlab Code
Using an initial set of parameters, the system of three ODEs was used to solve for the unknown
variables. These initial conditions were set for the dependent variables:

ht=0 = 0
Vc t=0 = 0
xt=0 = 0
Next, a script was created to solve the system of ODEs using the built-in MATLAB function
ode45. (The actual script can be found in the appendix) Here, the design parameters and the
calibration parameters were defined and given values were input in order to solve for the
dependent variables in the ODEs. Also, an initial conditions vector and a timespan vector were
defined so that the MATLAB program would perform ode45 over a given time interval. Lastly, a
new function file was created for use in the ode45 built-in function to help evaluate the three
differential equations.
The calibration parameters used in the MATLAB script were chosen based on the data and times
we recorded during the test run of our cart. In order to accurately predict the time our cart took to
cross 50ft at a 2% grade, we had to adjust our calibration parameters accordingly. These
calibration parameters included the drag and friction coefficients, which helped reduce the
velocity of our cart to zero. By only taking into account the effects of gravity, our cart would
have taken a very large amount of time for velocity to reach zero; therefore we manipulated the
drag and friction coefficients.

8
After the program solved the ODEs, a plot of time versus each dependent variable was produced,
along with a plot of the jet velocity versus time:

From these results, we predicted that our cart would take 2.799 seconds to cross the finish line on
race day.

Tank Specifications
Diameter of tank (D)
Z1
s+h
L

12 in.
8.25 in.
25 in.
7.75 in.

Tank Options (Chosen Prior to Race)
d - diameter of nozzle
P – pressure
h – water height
t – time prediction

1 in.
55 psi
4in.
2.79 sec.
9
Cart Materials and Design
The chamber attached to the cart consists of a cone made of aluminum steel, riveted together on
opposite sides of the lateral area. The cone was attached to a typical skateboard with two
bearings and four wheels using four metal legs. The metal legs are bolted to the skateboard and
welded to the cone. This specific design was chosen because the cone shape has a low level of
aerodynamic resistance. Also, the goal was to have a chamber with a large volume so that
maximum water tank pressure could be used, which ideally would result in the fastest speed.
Cross section views of cart:

Profile view of cart:

10
Preliminary Cart Testing Results (Friday 11/15)
Pressure (psi) Water Height (in.)
Test 1
60
3.25
Test 2
55
4
Test 3
55
4
Test 4
55
4
Test 5
45
6
* Cart crashed before crossing finish line

Nozzle (in.)
1/2
1
1
1
1

Time (seconds)
None*
2.71
2.79
None*
None*

During the preliminary cart test, we completed 5 test runs before the 15 minute time limit was
reached. Each of the 5, except tests 2 and 3, varied from one another. Test 1 was performed at a
pressure of 60 psi and a corresponding water height of 3.25 inches. The first test was done with
the 2nd smallest nozzle and failed to reach the finish line. The problem with the first test was
mainly attributed to the nozzle size and for further tests; the largest nozzle size was used.
For the second and third tests, the group decided on a pressure of 55 psi and a corresponding
water height of 4 inches. After the pressurized water was released, the cap detached from the end
of the cone. This helped release some pressure and water and helped the cart stay on track
without tipping over, but it did not help us achieve the fastest time. After two successful runs, the
group decided to tape the cap of the cone shut to achieve optimal time. Both test 4 and 5 were
unsuccessful due to the cart tipping over.
We realized the reason why our cart kept tipping over was because so much weight from the
water was building up in the tip of our cone and the creating a moment. That is why our cart was
only successful when the end cap popped off. This, along with the fact that the cart’s center of
gravity was closer to the front end, caused a moment at the front end of the cart and caused the
cart to tip over whenever the cap stayed on. In order to counteract this, we decided to try adding
a bowl to our final design. The bowl would be attached to the inside of the cone, causing more
weight to be added toward the back of the cone and causing the water jet to hit the cart farther
back.

11
Final Cart Race Results (Wednesday 11/27)
Pressure (psi) Water Height (in.)
Test 1
55
4
Test 2
55
4
Test 3
55
4
Test 4
55
4
Test 5
45
6
Test 6
45
6
* Cart crashed before crossing finish line

Nozzle (in.)
1
1
1
1
1
1

Time (seconds)
None*
3.09
None*
None*
3.90
None*

Test 1 was performed with a metal bowl attached to the inside of our cart. We lined the inside of
our cart with a trash bag and taped it to the outer edge and to the bowl to help keep the bowl in
place and make sure no water could get inside the cone. Our cart tipped over during test 1
because the pressure we specified wasn’t meant for the bowl design and it was too high.
For test 2 we took the bowl out and the cap popped off of the cone like it did in the test runs. The
cart made it across the finish line in 3.09 seconds which is only 0.3 seconds off from our
predicted time of 2.79 seconds. For tests 3 and 4 we left the bowl out again. Our cart wasn’t
tipping over this time, but it kept veering off to the side instead of staying on track.
For the 5th test, we decided to add the bowl again and reduce the pressure to 45 psi. During test 5
the cart made it across the finish line in 3.9 seconds, but during test 6 it flipped over again.
Overall, our cart only worked when the cap popped off because of the flaws in our design.
Because the cart was too heavy at the front end and because the skateboard was so small
compared to the cone, our cart was very unstable. Even if we had fixed the problems with our
cart and got it to go straight across the finish line without tipping over or having the cap pop off,
we still most likely wouldn’t have gotten the fastest time since the materials of the cart were so
heavy.

12
Race Videos and Pictures
Race Video:

http://www.youtube.com/watch?v=lZN4Dj4QmcQ&feature=c4overview&list=UUY_Dpnug5Jui2w-NLSP1JNQ
Figure of cart with bowl taped inside and trash bag attached:

13
Appendix
Matlab Code:

14
15
16
Resources
1. Sanders, Prof. B.F.. Water Jet Cart Analysis, CEE170 Class Website. 2012.
2. White, F.M.. Fluid Mechanics, 7th Edition, McGraw Hill 2011.

17

More Related Content

What's hot

Bachman_DFIT_2016-10-26_ForPublication
Bachman_DFIT_2016-10-26_ForPublicationBachman_DFIT_2016-10-26_ForPublication
Bachman_DFIT_2016-10-26_ForPublicationRobert Bachman
 
Fast Fluid Thermodynamics Simulation By Solving Heat Diffusion Equation
Fast Fluid Thermodynamics Simulation By Solving Heat Diffusion EquationFast Fluid Thermodynamics Simulation By Solving Heat Diffusion Equation
Fast Fluid Thermodynamics Simulation By Solving Heat Diffusion Equationijcga
 
Rudder Control Analysis / Hydraulic Pump Analysis
Rudder Control Analysis / Hydraulic Pump AnalysisRudder Control Analysis / Hydraulic Pump Analysis
Rudder Control Analysis / Hydraulic Pump AnalysisAndrè G. Odu
 
SPE174454_2015-06-08_1
SPE174454_2015-06-08_1SPE174454_2015-06-08_1
SPE174454_2015-06-08_1Robert Bachman
 
Pipeline engineering gas
Pipeline engineering  gasPipeline engineering  gas
Pipeline engineering gasoghogho_asemota
 
ODDLS: Overlapping domain decomposition Level Set Method
ODDLS: Overlapping domain decomposition Level Set MethodODDLS: Overlapping domain decomposition Level Set Method
ODDLS: Overlapping domain decomposition Level Set MethodAleix Valls
 
Chapter7gaschromatograph 110507221015-phpapp01
Chapter7gaschromatograph 110507221015-phpapp01Chapter7gaschromatograph 110507221015-phpapp01
Chapter7gaschromatograph 110507221015-phpapp01Cleophas Rwemera
 
Unit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTS
Unit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTSUnit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTS
Unit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTSsureshkcet
 
ME6604 GAS DYNAMICS AND JET PROPULSION NOTES
ME6604 GAS DYNAMICS AND JET PROPULSION NOTESME6604 GAS DYNAMICS AND JET PROPULSION NOTES
ME6604 GAS DYNAMICS AND JET PROPULSION NOTESBIBIN CHIDAMBARANATHAN
 
ME6604 GAS DYNAMICS AND JET PROPULSION SHORT QUESTION AND ANSWERS
ME6604 GAS DYNAMICS AND JET PROPULSION SHORT QUESTION AND ANSWERSME6604 GAS DYNAMICS AND JET PROPULSION SHORT QUESTION AND ANSWERS
ME6604 GAS DYNAMICS AND JET PROPULSION SHORT QUESTION AND ANSWERSBIBIN CHIDAMBARANATHAN
 
J2006 termodinamik 1 unit4
J2006 termodinamik 1 unit4J2006 termodinamik 1 unit4
J2006 termodinamik 1 unit4Malaysia
 
Nasa tech briefs ksk 11495, simplified model of duct flow
Nasa tech briefs ksk 11495, simplified model of duct flowNasa tech briefs ksk 11495, simplified model of duct flow
Nasa tech briefs ksk 11495, simplified model of duct flowJulio Banks
 
Offshore well intermediate
Offshore well intermediateOffshore well intermediate
Offshore well intermediateG.Balachandran
 

What's hot (19)

Bachman_DFIT_2016-10-26_ForPublication
Bachman_DFIT_2016-10-26_ForPublicationBachman_DFIT_2016-10-26_ForPublication
Bachman_DFIT_2016-10-26_ForPublication
 
Fast Fluid Thermodynamics Simulation By Solving Heat Diffusion Equation
Fast Fluid Thermodynamics Simulation By Solving Heat Diffusion EquationFast Fluid Thermodynamics Simulation By Solving Heat Diffusion Equation
Fast Fluid Thermodynamics Simulation By Solving Heat Diffusion Equation
 
Rudder Control Analysis / Hydraulic Pump Analysis
Rudder Control Analysis / Hydraulic Pump AnalysisRudder Control Analysis / Hydraulic Pump Analysis
Rudder Control Analysis / Hydraulic Pump Analysis
 
SPE174454_2015-06-08_1
SPE174454_2015-06-08_1SPE174454_2015-06-08_1
SPE174454_2015-06-08_1
 
@Pipeflow
@Pipeflow@Pipeflow
@Pipeflow
 
Pipeline engineering gas
Pipeline engineering  gasPipeline engineering  gas
Pipeline engineering gas
 
ODDLS: Overlapping domain decomposition Level Set Method
ODDLS: Overlapping domain decomposition Level Set MethodODDLS: Overlapping domain decomposition Level Set Method
ODDLS: Overlapping domain decomposition Level Set Method
 
Chapter7gaschromatograph 110507221015-phpapp01
Chapter7gaschromatograph 110507221015-phpapp01Chapter7gaschromatograph 110507221015-phpapp01
Chapter7gaschromatograph 110507221015-phpapp01
 
Unit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTS
Unit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTSUnit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTS
Unit - I BASIC CONCEPTS AND ISENTROPIC FLOW IN VARIABLE AREA DUCTS
 
Fm lab manual
Fm lab manualFm lab manual
Fm lab manual
 
ME6604 GAS DYNAMICS AND JET PROPULSION NOTES
ME6604 GAS DYNAMICS AND JET PROPULSION NOTESME6604 GAS DYNAMICS AND JET PROPULSION NOTES
ME6604 GAS DYNAMICS AND JET PROPULSION NOTES
 
PROBLEMA 3
PROBLEMA 3 PROBLEMA 3
PROBLEMA 3
 
EJERCICIO 2
EJERCICIO 2EJERCICIO 2
EJERCICIO 2
 
ME6604 GAS DYNAMICS AND JET PROPULSION SHORT QUESTION AND ANSWERS
ME6604 GAS DYNAMICS AND JET PROPULSION SHORT QUESTION AND ANSWERSME6604 GAS DYNAMICS AND JET PROPULSION SHORT QUESTION AND ANSWERS
ME6604 GAS DYNAMICS AND JET PROPULSION SHORT QUESTION AND ANSWERS
 
J2006 termodinamik 1 unit4
J2006 termodinamik 1 unit4J2006 termodinamik 1 unit4
J2006 termodinamik 1 unit4
 
Compressible Flow
Compressible FlowCompressible Flow
Compressible Flow
 
Nasa tech briefs ksk 11495, simplified model of duct flow
Nasa tech briefs ksk 11495, simplified model of duct flowNasa tech briefs ksk 11495, simplified model of duct flow
Nasa tech briefs ksk 11495, simplified model of duct flow
 
Unit4
Unit4Unit4
Unit4
 
Offshore well intermediate
Offshore well intermediateOffshore well intermediate
Offshore well intermediate
 

Similar to Intro to Fluid Mechanics Design Project

Fluid flow rate Experiment No. 5.pdf
Fluid flow rate Experiment No. 5.pdfFluid flow rate Experiment No. 5.pdf
Fluid flow rate Experiment No. 5.pdfKaiwan B. Hamasalih
 
Study of a Gear-Rack and links System: Equations, configuration and CAD design
Study of a Gear-Rack and links System: Equations, configuration and CAD designStudy of a Gear-Rack and links System: Equations, configuration and CAD design
Study of a Gear-Rack and links System: Equations, configuration and CAD designPietro Galli
 
Multi-Fidelity Optimization of a High Speed, Foil-Assisted Catamaran for Low ...
Multi-Fidelity Optimization of a High Speed, Foil-Assisted Catamaran for Low ...Multi-Fidelity Optimization of a High Speed, Foil-Assisted Catamaran for Low ...
Multi-Fidelity Optimization of a High Speed, Foil-Assisted Catamaran for Low ...Kellen Betts
 
Methods to determine pressure drop in an evaporator or a condenser
Methods to determine pressure drop in an evaporator or a condenserMethods to determine pressure drop in an evaporator or a condenser
Methods to determine pressure drop in an evaporator or a condenserTony Yen
 
The optimal control system of the ship based on the linear quadratic regular ...
The optimal control system of the ship based on the linear quadratic regular ...The optimal control system of the ship based on the linear quadratic regular ...
The optimal control system of the ship based on the linear quadratic regular ...IJECEIAES
 
B_B1_G3_CP_HMAFP.pptx
B_B1_G3_CP_HMAFP.pptxB_B1_G3_CP_HMAFP.pptx
B_B1_G3_CP_HMAFP.pptxKhaireSushom
 
A practical approach to design and optimization of single phase liquid to liq...
A practical approach to design and optimization of single phase liquid to liq...A practical approach to design and optimization of single phase liquid to liq...
A practical approach to design and optimization of single phase liquid to liq...iaemedu
 
Fm sol chap06 044
Fm sol chap06 044Fm sol chap06 044
Fm sol chap06 044erenkeceli
 
Transient three dimensional cfd modelling of ceilng fan
Transient three dimensional cfd modelling of ceilng fanTransient three dimensional cfd modelling of ceilng fan
Transient three dimensional cfd modelling of ceilng fanLahiru Dilshan
 
"Design Criteria of Lift Irrigation Scheme"
"Design Criteria of Lift Irrigation Scheme""Design Criteria of Lift Irrigation Scheme"
"Design Criteria of Lift Irrigation Scheme"IRJET Journal
 
PORT FLOW SIMULATION OF AN IC ENGINE
PORT FLOW SIMULATION OF AN IC ENGINEPORT FLOW SIMULATION OF AN IC ENGINE
PORT FLOW SIMULATION OF AN IC ENGINEijiert bestjournal
 
Head Loss Estimation for Water Jets from Flip Buckets
Head Loss Estimation for Water Jets from Flip BucketsHead Loss Estimation for Water Jets from Flip Buckets
Head Loss Estimation for Water Jets from Flip Bucketstheijes
 

Similar to Intro to Fluid Mechanics Design Project (20)

Problema 5
Problema 5Problema 5
Problema 5
 
Flow in Pipes
Flow in PipesFlow in Pipes
Flow in Pipes
 
Momentum equation.pdf
 Momentum equation.pdf Momentum equation.pdf
Momentum equation.pdf
 
Fluid flow rate Experiment No. 5.pdf
Fluid flow rate Experiment No. 5.pdfFluid flow rate Experiment No. 5.pdf
Fluid flow rate Experiment No. 5.pdf
 
Fo ode-1
Fo ode-1Fo ode-1
Fo ode-1
 
Study of a Gear-Rack and links System: Equations, configuration and CAD design
Study of a Gear-Rack and links System: Equations, configuration and CAD designStudy of a Gear-Rack and links System: Equations, configuration and CAD design
Study of a Gear-Rack and links System: Equations, configuration and CAD design
 
Multi-Fidelity Optimization of a High Speed, Foil-Assisted Catamaran for Low ...
Multi-Fidelity Optimization of a High Speed, Foil-Assisted Catamaran for Low ...Multi-Fidelity Optimization of a High Speed, Foil-Assisted Catamaran for Low ...
Multi-Fidelity Optimization of a High Speed, Foil-Assisted Catamaran for Low ...
 
Final Report 4_22_15
Final Report 4_22_15Final Report 4_22_15
Final Report 4_22_15
 
Methods to determine pressure drop in an evaporator or a condenser
Methods to determine pressure drop in an evaporator or a condenserMethods to determine pressure drop in an evaporator or a condenser
Methods to determine pressure drop in an evaporator or a condenser
 
Power2010_27048_Final
Power2010_27048_FinalPower2010_27048_Final
Power2010_27048_Final
 
The optimal control system of the ship based on the linear quadratic regular ...
The optimal control system of the ship based on the linear quadratic regular ...The optimal control system of the ship based on the linear quadratic regular ...
The optimal control system of the ship based on the linear quadratic regular ...
 
Problema 4
Problema 4Problema 4
Problema 4
 
Fluid Mechanics report
Fluid Mechanics reportFluid Mechanics report
Fluid Mechanics report
 
B_B1_G3_CP_HMAFP.pptx
B_B1_G3_CP_HMAFP.pptxB_B1_G3_CP_HMAFP.pptx
B_B1_G3_CP_HMAFP.pptx
 
A practical approach to design and optimization of single phase liquid to liq...
A practical approach to design and optimization of single phase liquid to liq...A practical approach to design and optimization of single phase liquid to liq...
A practical approach to design and optimization of single phase liquid to liq...
 
Fm sol chap06 044
Fm sol chap06 044Fm sol chap06 044
Fm sol chap06 044
 
Transient three dimensional cfd modelling of ceilng fan
Transient three dimensional cfd modelling of ceilng fanTransient three dimensional cfd modelling of ceilng fan
Transient three dimensional cfd modelling of ceilng fan
 
"Design Criteria of Lift Irrigation Scheme"
"Design Criteria of Lift Irrigation Scheme""Design Criteria of Lift Irrigation Scheme"
"Design Criteria of Lift Irrigation Scheme"
 
PORT FLOW SIMULATION OF AN IC ENGINE
PORT FLOW SIMULATION OF AN IC ENGINEPORT FLOW SIMULATION OF AN IC ENGINE
PORT FLOW SIMULATION OF AN IC ENGINE
 
Head Loss Estimation for Water Jets from Flip Buckets
Head Loss Estimation for Water Jets from Flip BucketsHead Loss Estimation for Water Jets from Flip Buckets
Head Loss Estimation for Water Jets from Flip Buckets
 

More from Megan Hanrahan

Transportation Systems Design Project
Transportation Systems Design ProjectTransportation Systems Design Project
Transportation Systems Design ProjectMegan Hanrahan
 
CEE81B AutoCAD Practice
CEE81B AutoCAD PracticeCEE81B AutoCAD Practice
CEE81B AutoCAD PracticeMegan Hanrahan
 
CEE81B Introduction to ArcGIS
CEE81B Introduction to ArcGISCEE81B Introduction to ArcGIS
CEE81B Introduction to ArcGISMegan Hanrahan
 

More from Megan Hanrahan (6)

CEE171 Final Project
CEE171  Final ProjectCEE171  Final Project
CEE171 Final Project
 
Transportation Systems Design Project
Transportation Systems Design ProjectTransportation Systems Design Project
Transportation Systems Design Project
 
CEE81B AutoCAD Practice
CEE81B AutoCAD PracticeCEE81B AutoCAD Practice
CEE81B AutoCAD Practice
 
CEE81B Introduction to ArcGIS
CEE81B Introduction to ArcGISCEE81B Introduction to ArcGIS
CEE81B Introduction to ArcGIS
 
CEE81A Homework 2
CEE81A Homework 2CEE81A Homework 2
CEE81A Homework 2
 
First AutoCAD Project
First AutoCAD ProjectFirst AutoCAD Project
First AutoCAD Project
 

Recently uploaded

MENTAL STATUS EXAMINATION format.docx
MENTAL     STATUS EXAMINATION format.docxMENTAL     STATUS EXAMINATION format.docx
MENTAL STATUS EXAMINATION format.docxPoojaSen20
 
URLs and Routing in the Odoo 17 Website App
URLs and Routing in the Odoo 17 Website AppURLs and Routing in the Odoo 17 Website App
URLs and Routing in the Odoo 17 Website AppCeline George
 
Grant Readiness 101 TechSoup and Remy Consulting
Grant Readiness 101 TechSoup and Remy ConsultingGrant Readiness 101 TechSoup and Remy Consulting
Grant Readiness 101 TechSoup and Remy ConsultingTechSoup
 
Contemporary philippine arts from the regions_PPT_Module_12 [Autosaved] (1).pptx
Contemporary philippine arts from the regions_PPT_Module_12 [Autosaved] (1).pptxContemporary philippine arts from the regions_PPT_Module_12 [Autosaved] (1).pptx
Contemporary philippine arts from the regions_PPT_Module_12 [Autosaved] (1).pptxRoyAbrique
 
18-04-UA_REPORT_MEDIALITERAСY_INDEX-DM_23-1-final-eng.pdf
18-04-UA_REPORT_MEDIALITERAСY_INDEX-DM_23-1-final-eng.pdf18-04-UA_REPORT_MEDIALITERAСY_INDEX-DM_23-1-final-eng.pdf
18-04-UA_REPORT_MEDIALITERAСY_INDEX-DM_23-1-final-eng.pdfssuser54595a
 
Call Girls in Dwarka Mor Delhi Contact Us 9654467111
Call Girls in Dwarka Mor Delhi Contact Us 9654467111Call Girls in Dwarka Mor Delhi Contact Us 9654467111
Call Girls in Dwarka Mor Delhi Contact Us 9654467111Sapana Sha
 
mini mental status format.docx
mini    mental       status     format.docxmini    mental       status     format.docx
mini mental status format.docxPoojaSen20
 
Kisan Call Centre - To harness potential of ICT in Agriculture by answer farm...
Kisan Call Centre - To harness potential of ICT in Agriculture by answer farm...Kisan Call Centre - To harness potential of ICT in Agriculture by answer farm...
Kisan Call Centre - To harness potential of ICT in Agriculture by answer farm...Krashi Coaching
 
Mastering the Unannounced Regulatory Inspection
Mastering the Unannounced Regulatory InspectionMastering the Unannounced Regulatory Inspection
Mastering the Unannounced Regulatory InspectionSafetyChain Software
 
Concept of Vouching. B.Com(Hons) /B.Compdf
Concept of Vouching. B.Com(Hons) /B.CompdfConcept of Vouching. B.Com(Hons) /B.Compdf
Concept of Vouching. B.Com(Hons) /B.CompdfUmakantAnnand
 
Introduction to ArtificiaI Intelligence in Higher Education
Introduction to ArtificiaI Intelligence in Higher EducationIntroduction to ArtificiaI Intelligence in Higher Education
Introduction to ArtificiaI Intelligence in Higher Educationpboyjonauth
 
_Math 4-Q4 Week 5.pptx Steps in Collecting Data
_Math 4-Q4 Week 5.pptx Steps in Collecting Data_Math 4-Q4 Week 5.pptx Steps in Collecting Data
_Math 4-Q4 Week 5.pptx Steps in Collecting DataJhengPantaleon
 
Hybridoma Technology ( Production , Purification , and Application )
Hybridoma Technology  ( Production , Purification , and Application  ) Hybridoma Technology  ( Production , Purification , and Application  )
Hybridoma Technology ( Production , Purification , and Application ) Sakshi Ghasle
 
How to Make a Pirate ship Primary Education.pptx
How to Make a Pirate ship Primary Education.pptxHow to Make a Pirate ship Primary Education.pptx
How to Make a Pirate ship Primary Education.pptxmanuelaromero2013
 
Accessible design: Minimum effort, maximum impact
Accessible design: Minimum effort, maximum impactAccessible design: Minimum effort, maximum impact
Accessible design: Minimum effort, maximum impactdawncurless
 
POINT- BIOCHEMISTRY SEM 2 ENZYMES UNIT 5.pptx
POINT- BIOCHEMISTRY SEM 2 ENZYMES UNIT 5.pptxPOINT- BIOCHEMISTRY SEM 2 ENZYMES UNIT 5.pptx
POINT- BIOCHEMISTRY SEM 2 ENZYMES UNIT 5.pptxSayali Powar
 
Industrial Policy - 1948, 1956, 1973, 1977, 1980, 1991
Industrial Policy - 1948, 1956, 1973, 1977, 1980, 1991Industrial Policy - 1948, 1956, 1973, 1977, 1980, 1991
Industrial Policy - 1948, 1956, 1973, 1977, 1980, 1991RKavithamani
 
Introduction to AI in Higher Education_draft.pptx
Introduction to AI in Higher Education_draft.pptxIntroduction to AI in Higher Education_draft.pptx
Introduction to AI in Higher Education_draft.pptxpboyjonauth
 

Recently uploaded (20)

MENTAL STATUS EXAMINATION format.docx
MENTAL     STATUS EXAMINATION format.docxMENTAL     STATUS EXAMINATION format.docx
MENTAL STATUS EXAMINATION format.docx
 
Código Creativo y Arte de Software | Unidad 1
Código Creativo y Arte de Software | Unidad 1Código Creativo y Arte de Software | Unidad 1
Código Creativo y Arte de Software | Unidad 1
 
URLs and Routing in the Odoo 17 Website App
URLs and Routing in the Odoo 17 Website AppURLs and Routing in the Odoo 17 Website App
URLs and Routing in the Odoo 17 Website App
 
Grant Readiness 101 TechSoup and Remy Consulting
Grant Readiness 101 TechSoup and Remy ConsultingGrant Readiness 101 TechSoup and Remy Consulting
Grant Readiness 101 TechSoup and Remy Consulting
 
Contemporary philippine arts from the regions_PPT_Module_12 [Autosaved] (1).pptx
Contemporary philippine arts from the regions_PPT_Module_12 [Autosaved] (1).pptxContemporary philippine arts from the regions_PPT_Module_12 [Autosaved] (1).pptx
Contemporary philippine arts from the regions_PPT_Module_12 [Autosaved] (1).pptx
 
18-04-UA_REPORT_MEDIALITERAСY_INDEX-DM_23-1-final-eng.pdf
18-04-UA_REPORT_MEDIALITERAСY_INDEX-DM_23-1-final-eng.pdf18-04-UA_REPORT_MEDIALITERAСY_INDEX-DM_23-1-final-eng.pdf
18-04-UA_REPORT_MEDIALITERAСY_INDEX-DM_23-1-final-eng.pdf
 
Call Girls in Dwarka Mor Delhi Contact Us 9654467111
Call Girls in Dwarka Mor Delhi Contact Us 9654467111Call Girls in Dwarka Mor Delhi Contact Us 9654467111
Call Girls in Dwarka Mor Delhi Contact Us 9654467111
 
Staff of Color (SOC) Retention Efforts DDSD
Staff of Color (SOC) Retention Efforts DDSDStaff of Color (SOC) Retention Efforts DDSD
Staff of Color (SOC) Retention Efforts DDSD
 
mini mental status format.docx
mini    mental       status     format.docxmini    mental       status     format.docx
mini mental status format.docx
 
Kisan Call Centre - To harness potential of ICT in Agriculture by answer farm...
Kisan Call Centre - To harness potential of ICT in Agriculture by answer farm...Kisan Call Centre - To harness potential of ICT in Agriculture by answer farm...
Kisan Call Centre - To harness potential of ICT in Agriculture by answer farm...
 
Mastering the Unannounced Regulatory Inspection
Mastering the Unannounced Regulatory InspectionMastering the Unannounced Regulatory Inspection
Mastering the Unannounced Regulatory Inspection
 
Concept of Vouching. B.Com(Hons) /B.Compdf
Concept of Vouching. B.Com(Hons) /B.CompdfConcept of Vouching. B.Com(Hons) /B.Compdf
Concept of Vouching. B.Com(Hons) /B.Compdf
 
Introduction to ArtificiaI Intelligence in Higher Education
Introduction to ArtificiaI Intelligence in Higher EducationIntroduction to ArtificiaI Intelligence in Higher Education
Introduction to ArtificiaI Intelligence in Higher Education
 
_Math 4-Q4 Week 5.pptx Steps in Collecting Data
_Math 4-Q4 Week 5.pptx Steps in Collecting Data_Math 4-Q4 Week 5.pptx Steps in Collecting Data
_Math 4-Q4 Week 5.pptx Steps in Collecting Data
 
Hybridoma Technology ( Production , Purification , and Application )
Hybridoma Technology  ( Production , Purification , and Application  ) Hybridoma Technology  ( Production , Purification , and Application  )
Hybridoma Technology ( Production , Purification , and Application )
 
How to Make a Pirate ship Primary Education.pptx
How to Make a Pirate ship Primary Education.pptxHow to Make a Pirate ship Primary Education.pptx
How to Make a Pirate ship Primary Education.pptx
 
Accessible design: Minimum effort, maximum impact
Accessible design: Minimum effort, maximum impactAccessible design: Minimum effort, maximum impact
Accessible design: Minimum effort, maximum impact
 
POINT- BIOCHEMISTRY SEM 2 ENZYMES UNIT 5.pptx
POINT- BIOCHEMISTRY SEM 2 ENZYMES UNIT 5.pptxPOINT- BIOCHEMISTRY SEM 2 ENZYMES UNIT 5.pptx
POINT- BIOCHEMISTRY SEM 2 ENZYMES UNIT 5.pptx
 
Industrial Policy - 1948, 1956, 1973, 1977, 1980, 1991
Industrial Policy - 1948, 1956, 1973, 1977, 1980, 1991Industrial Policy - 1948, 1956, 1973, 1977, 1980, 1991
Industrial Policy - 1948, 1956, 1973, 1977, 1980, 1991
 
Introduction to AI in Higher Education_draft.pptx
Introduction to AI in Higher Education_draft.pptxIntroduction to AI in Higher Education_draft.pptx
Introduction to AI in Higher Education_draft.pptx
 

Intro to Fluid Mechanics Design Project

  • 1. CEE170: Introduction to Fluid Mechanics Water Jet Cart Design Project Group 18: Top Crew Chosita Sribhibhadh Kevin Krik Patricia Kharazmi Megan Hanrahan Saman Shaolian Ali Behbahani Toni Lynch 1
  • 2. Table of Contents Section Title Page Number Introduction…………………………………………………………… 3 Predicting the Velocity of the Water Jet………..…………………….. 3 Predicting the Rate of Change of Tank Water Height over Time….…. 6 Predicting the Speed of the Cart............................................................. 7 Predicting the Distance the Cart Will Travel…….…………………… 8 The Matlab Code……………………………………………………… 8 Tank Options and Specifications……………………………..……...... 9 Cart Materials and Design……………....…………………………..... 10 Preliminary Cart Testing Results…………………………….……….. 11 Final Cart Race Results……………………………………………….. 12 Race Videos and Pictures.…………………………………………….. 13 Appendix…………………………………………………………….… 14 Resources……………………………………………………………… 17 2
  • 3. Introduction The purpose of this project is to design a cart that can travel a 50 foot distance along a 2% slope with a high speed. Each group should be able to predict the speed of their cart based on Matlab modeling and calibration of these models due to preliminary testing. The goal of the project is to design a cart with the fastest design speed or have the closest prediction of time using the test data and Matlab model. Provided is a pressurized tank filled with water. The tank has a nozzle of interchangeable diameter that will shoot out a jet of water. The teams’ job is to design a chamber to attach to the cart that will catch the water jet and use it to propel the cart forward and to choose certain tank specifications that will lead to a successful run. Predicting the Velocity of the Water Jet The energy equation, which comes from conservation of energy in the Reynolds Transport Theorem is used to find the velocity of the water jet. Here is how the equation used is derived: Sketch of pressurized tank: 2 𝑃1 𝑉12 𝑃2 𝑉2 + + 𝑍1 + ℎ 𝑝 = + + 𝑍2 + ℎ 𝑡 + ℎ 𝐿 𝛾 2𝑔 𝛾 2𝑔 3
  • 4.            P1 is the pressure in the tank, which can be denoted as P γ is the density of water (ρ=998 kg/m3) multiplied by the acceleration of gravity (g=9.81 m/s2) V1 is the velocity of the water in the tank, which is such a small number, it can be considered zero Z1 is the height of water in the tank P2 is the pressure at point 2 and since it is open to the atmosphere, it can also be consider zero V2 is the velocity of the water jet which can be denoted as VJ Z2 is the height of the centerline of the nozzle hp is the height of energy gained due to a pump, but since there is no pump, it equals zero ht is the height of energy removed from the system by a turbine, this term also equals zero hL is the height of energy lost due to friction in the nozzle A new variable h is used to represent the height of the water in the tank to the centerline of the nozzle where: ℎ = 𝑍1 − 𝑍2 Taking all these factors into account, the equation is then simplified to: 𝑉𝐽2 𝑃 +ℎ = +ℎ𝐿 𝛾 2𝑔 𝐿 where ℎ 𝐿 = (𝐾𝑣 + 𝑓 ) 2 𝑉𝐽 𝑑 2𝑔     Kv is the minor loss coefficient 𝑓 is the friction factor L is the length of the nozzle d is the diameter of the nozzle The simplified energy equation now becomes: 𝑉𝐽2 𝑃 𝐿 +ℎ= (1 + 𝐾 + 𝑓 ) 𝛾 2𝑔 𝑑 Finally, solving for VJ results in the equation: 𝑃 2𝑔 ( 𝛾 + ℎ) 𝑉𝐽 = √ 𝐿 1+ 𝐾+ 𝑓 𝑑 4
  • 5. The equation that accounts for the change in pressure in the tank over time is: 𝑘 𝑠 ) 𝑃 = 𝑃0 ( 𝑠 + ℎ0 + ℎ    P0 is initial pressure in the tank s is the initial height from the top of the tank to the water in the tank h0 is the initial height of water in the tank  k is the ratio of specific heats inside and outside of the tank This equation must be plugged into the equation for VJ for accuracy: 𝑘 𝑠 ) 𝑃0 ( 𝑠 + ℎ0 + ℎ 2𝑔 ( + ℎ) 𝛾 𝑉𝐽 = √ 1+ 𝐾+ 𝑓 𝐿 𝑑 5
  • 6. Predicting the Rate of Change of Tank Water Height over Time Now that the velocity of the water jet has been estimated, it can be used to estimate the rate at which the height of the water in the tank changes over time. The volume of water changing in the tank over time can be expressed as: 𝑑𝑉 𝑡𝑎𝑛𝑘 = −𝑄 𝑜𝑢𝑡 𝑑𝑡  Qout is the flow of water out of the tank (A2V2) which can be written as: 𝑄 𝑜𝑢𝑡 = 𝜋 2 𝑑 𝑉𝐽 4 Since the diameter of the tank always remains constant, the expression for the change in volume of the tank can be written as: 𝑑𝑉 𝑡𝑎𝑛𝑘 𝜋 𝑑ℎ = 𝐷2 𝑑𝑡 4 𝑑𝑡  D is the diameter of the tank  dh/dt is the change in height of the water over time Substituting these two equations into the original results in: 𝜋 2 𝑑ℎ 𝜋 𝐷 = − 𝑑 2 𝑉𝐽 4 𝑑𝑡 4 Solving for dh/dt gives: 𝑑ℎ 𝑑2 = (− 2 𝑉𝐽 ) 𝑑𝑡 𝐷 Plugging the jet velocity equation into this equation supplies the first ordinary differential equation (ODE) that will be solved in Matlab: 𝑘 𝑠𝑜 2∗(𝑔∗ℎ+(𝑃𝑜∗( 𝑠𝑜+ℎ𝑜−ℎ) )) ( 𝑑ℎ 𝑑2 =− 2∗ 𝑑𝑡 𝐷 𝑝 0.5 ) 𝐿 1 + 𝐾𝑣 + 𝑓 ∗ ( ) 𝑑 ( ) 6
  • 7. Predicting the Speed of the Cart Once the velocity of the water jet has been predicted, that value, along with the dimensions of the cart design can be used to predict the speed of the cart. The prediction of the cart’s speed comes from Newton’s Second Law of Motion Equation (Σ𝐹 = 𝑚𝑎). Accounting for all the forces acting on the cart gives the equation: 𝐹𝐽 − 𝐹 𝐺 − 𝐹 𝑅 = 𝑚𝑎 Solving the equation for acceleration gives: 𝑎=  𝐹𝐽 − 𝐹 𝐺 − 𝐹 𝑅 𝑚 FJ is the force exerted on the cart by the jet, which can be written as: 𝐹𝐽 = 𝛼𝜌𝐴 𝐽 𝑉 2 𝑅 o α is the momentum transfer coefficient (calibration parameter from 0-2) o AJ is the area of the water jet (π/4*d2) o VR is the relative velocity between the jet and the cart (V J-VC)  FG is the gravitational force on the cart which can be written as: 𝐹 𝐺 = 𝑚𝑔𝑠𝑖𝑛𝜃 o θ is the angle of incline o m is the mass of the cart  FR is the force due to rolling friction and air resistance which can be ignored in further calculations Plugging all of these forces into Newton’s Equation solved for acceleration gives: 𝛼𝜌𝐴 𝐽 𝑉 2 𝑅 𝑎= − 𝑔𝑠𝑖𝑛𝜃 𝑚 Knowing that acceleration is the change in velocity over time (𝑎 = rewritten as: 𝑑𝑉 𝑐 𝑑𝑡 ), this equation can be 𝛼𝜌𝐴 𝐽 𝑉 2 𝑑𝑉 𝐶 𝑅 = − 𝑔𝑠𝑖𝑛𝜃 𝑑𝑡 𝑚 Accounting for deceleration due to drag and friction (Cdf) supplies the second ODE to be solved in Matlab: 𝛼𝜌𝐴 𝐽 𝑉 2 𝑑𝑉 𝐶 𝑅 = − 𝑔𝑠𝑖𝑛𝜃 − 𝐶 𝑑𝑓 𝑑𝑡 𝑚 7
  • 8. Predicting the Distance the Cart Will Travel Now that the speed of the cart has been predicted, the distance it will travel can also be predicted. The total distance the cart will travel is simply the change in the cart’s velocity over time. This can be expressed as: 𝑑𝑥 = 𝑉𝑐 𝑑𝑡 Solving for velocity supplies the third ODE to be solved in Matlab: 𝑑𝑥 = 𝑉𝑐 𝑑𝑡 The Matlab Code Using an initial set of parameters, the system of three ODEs was used to solve for the unknown variables. These initial conditions were set for the dependent variables: ht=0 = 0 Vc t=0 = 0 xt=0 = 0 Next, a script was created to solve the system of ODEs using the built-in MATLAB function ode45. (The actual script can be found in the appendix) Here, the design parameters and the calibration parameters were defined and given values were input in order to solve for the dependent variables in the ODEs. Also, an initial conditions vector and a timespan vector were defined so that the MATLAB program would perform ode45 over a given time interval. Lastly, a new function file was created for use in the ode45 built-in function to help evaluate the three differential equations. The calibration parameters used in the MATLAB script were chosen based on the data and times we recorded during the test run of our cart. In order to accurately predict the time our cart took to cross 50ft at a 2% grade, we had to adjust our calibration parameters accordingly. These calibration parameters included the drag and friction coefficients, which helped reduce the velocity of our cart to zero. By only taking into account the effects of gravity, our cart would have taken a very large amount of time for velocity to reach zero; therefore we manipulated the drag and friction coefficients. 8
  • 9. After the program solved the ODEs, a plot of time versus each dependent variable was produced, along with a plot of the jet velocity versus time: From these results, we predicted that our cart would take 2.799 seconds to cross the finish line on race day. Tank Specifications Diameter of tank (D) Z1 s+h L 12 in. 8.25 in. 25 in. 7.75 in. Tank Options (Chosen Prior to Race) d - diameter of nozzle P – pressure h – water height t – time prediction 1 in. 55 psi 4in. 2.79 sec. 9
  • 10. Cart Materials and Design The chamber attached to the cart consists of a cone made of aluminum steel, riveted together on opposite sides of the lateral area. The cone was attached to a typical skateboard with two bearings and four wheels using four metal legs. The metal legs are bolted to the skateboard and welded to the cone. This specific design was chosen because the cone shape has a low level of aerodynamic resistance. Also, the goal was to have a chamber with a large volume so that maximum water tank pressure could be used, which ideally would result in the fastest speed. Cross section views of cart: Profile view of cart: 10
  • 11. Preliminary Cart Testing Results (Friday 11/15) Pressure (psi) Water Height (in.) Test 1 60 3.25 Test 2 55 4 Test 3 55 4 Test 4 55 4 Test 5 45 6 * Cart crashed before crossing finish line Nozzle (in.) 1/2 1 1 1 1 Time (seconds) None* 2.71 2.79 None* None* During the preliminary cart test, we completed 5 test runs before the 15 minute time limit was reached. Each of the 5, except tests 2 and 3, varied from one another. Test 1 was performed at a pressure of 60 psi and a corresponding water height of 3.25 inches. The first test was done with the 2nd smallest nozzle and failed to reach the finish line. The problem with the first test was mainly attributed to the nozzle size and for further tests; the largest nozzle size was used. For the second and third tests, the group decided on a pressure of 55 psi and a corresponding water height of 4 inches. After the pressurized water was released, the cap detached from the end of the cone. This helped release some pressure and water and helped the cart stay on track without tipping over, but it did not help us achieve the fastest time. After two successful runs, the group decided to tape the cap of the cone shut to achieve optimal time. Both test 4 and 5 were unsuccessful due to the cart tipping over. We realized the reason why our cart kept tipping over was because so much weight from the water was building up in the tip of our cone and the creating a moment. That is why our cart was only successful when the end cap popped off. This, along with the fact that the cart’s center of gravity was closer to the front end, caused a moment at the front end of the cart and caused the cart to tip over whenever the cap stayed on. In order to counteract this, we decided to try adding a bowl to our final design. The bowl would be attached to the inside of the cone, causing more weight to be added toward the back of the cone and causing the water jet to hit the cart farther back. 11
  • 12. Final Cart Race Results (Wednesday 11/27) Pressure (psi) Water Height (in.) Test 1 55 4 Test 2 55 4 Test 3 55 4 Test 4 55 4 Test 5 45 6 Test 6 45 6 * Cart crashed before crossing finish line Nozzle (in.) 1 1 1 1 1 1 Time (seconds) None* 3.09 None* None* 3.90 None* Test 1 was performed with a metal bowl attached to the inside of our cart. We lined the inside of our cart with a trash bag and taped it to the outer edge and to the bowl to help keep the bowl in place and make sure no water could get inside the cone. Our cart tipped over during test 1 because the pressure we specified wasn’t meant for the bowl design and it was too high. For test 2 we took the bowl out and the cap popped off of the cone like it did in the test runs. The cart made it across the finish line in 3.09 seconds which is only 0.3 seconds off from our predicted time of 2.79 seconds. For tests 3 and 4 we left the bowl out again. Our cart wasn’t tipping over this time, but it kept veering off to the side instead of staying on track. For the 5th test, we decided to add the bowl again and reduce the pressure to 45 psi. During test 5 the cart made it across the finish line in 3.9 seconds, but during test 6 it flipped over again. Overall, our cart only worked when the cap popped off because of the flaws in our design. Because the cart was too heavy at the front end and because the skateboard was so small compared to the cone, our cart was very unstable. Even if we had fixed the problems with our cart and got it to go straight across the finish line without tipping over or having the cap pop off, we still most likely wouldn’t have gotten the fastest time since the materials of the cart were so heavy. 12
  • 13. Race Videos and Pictures Race Video: http://www.youtube.com/watch?v=lZN4Dj4QmcQ&feature=c4overview&list=UUY_Dpnug5Jui2w-NLSP1JNQ Figure of cart with bowl taped inside and trash bag attached: 13
  • 15. 15
  • 16. 16
  • 17. Resources 1. Sanders, Prof. B.F.. Water Jet Cart Analysis, CEE170 Class Website. 2012. 2. White, F.M.. Fluid Mechanics, 7th Edition, McGraw Hill 2011. 17