SlideShare a Scribd company logo
1 of 10
Download to read offline
Mechanical Engineering 4J03
McMaster University
Project #2
Prepared For: Dr. Hamed
Date of Tutorial: March 6, 2015
Assignment Due Date: March 20, 2015
Prepared By: Shaun Chiasson, 1070043
Objective:
A cooling tank was to be examined for flow characteristics and pressure drop in order to
determine a means to stabilize the water velocity that passes the cooling chamber. A design
needed to be created that could bring the velocity at the chamber to a steady value within
specified values while having an unlimited pressure allowance. The final design was to include
the use of baffles and not change the tank in anyway.
Results:
From the given information in the problem the inlet velocity calculated was 0.673 m/s.
The initial grid size indicated was too small to work with so a grid ten times larger was used.
The original grid called for a 0.0007m mesh but instead a 0.007m mesh was used instead in order
to save computation time.
( ) ( )
Figure 1: Flow velocity vector plot for the case of no baffles installed.
Figure 2: Graph of velocity magnitudes for inspection lines A, B, and C for the case of no baffles installed.
Figure 3: Graph of pressure magnitudes for inspection lines A, and C for the case of no baffles installed.
Figure 4: First two attempts at a suitable baffle design.
Figure 5: Second set of two attempts at a suitable baffle design.
Figure 6: Third set of two attempts at a suitable baffle design.
Figure 6: Fourth set of two attempts at a suitable baffle design.
Figure 7: Fifth set of two attempts at a suitable baffle design.
Figure 8: Final baffle design velocity vector plot.
It is important to note that none of the designs tested would converge to the prescribed
1.0E-5 residual within the recommended three hundred iterations. Some designs did converge to
the standard residual of 1.0E-4 but did not meet the requirements of the project. There was also
sinusoidal variance in the residuals but not sufficient time to use double precision. Since none of
the solutions are sufficient to meet the requirements and convergence was not met a grid
independence test was not necessary. The final design presented here could meet the criteria
with more work on the proposed geometry and may converge to 1.0E-5 if more iterations were
allowed to run. The solution presented here has been resolved sufficiently well to conclude that
the design can be reworked into a successful configuration because the mesh had been refined in
the areas of the baffles where the gradients are highest as shown in Figure 9.
Figure 9: Final baffle design mesh used in the solver.
Figure 10: Graph of velocity magnitude for inspection line B for the final design.
Figure 11: Graph of pressure magnitudes for inspection lines A, and C for the final design.
Figure 12: Dimensions for the geometry of the final baffle design configuration.
Note: Only the minimum amounts of dimensions are shown and those not shown can be assumed to be the same as
others that are of the same magnitude and shown in the figure above.
Discussion:
The criterion for the velocity of the water states that an average of 80 fpm with a range of
plus or minus ten percent would be desirable. To interpret the graphs above these values needed
to be converted to meters per second.
( ) ( ) ( )
( )
( )
Figure 10 illustrates that a portion of the velocity magnitude graph lies within the range
specified. This portion of the graph is fairly close to the edge of the cooling chamber circle, and
this is the main reason to believe that with some minor alterations the final design could be made
to satisfy the design criteria. The average velocity over the whole inspection line B will now be
calculated from the graphs and compared to that of the case with no baffles installed.
̅
( )
̅
( )
̅ ̅
̅
( ) ( )
( )
The addition of the baffle system has had a big impact on the average velocity of the
water passing by inspection line B. This is the desired effect since the water initially enters the
tank at a velocity of 0.673 m/s it is necessary to try and slow it down a great deal in order to
attempt to reach the target velocity of 0.41 m/s. The addition of the baffles comes at a price
however; the pressure drop in the tank has increased and will now be examined.
( )
The calculations above indicate that for relatively small decreases in the average velocity
of the water a very large pressure drop will be required. This could mean that if more baffles are
inserted in an appropriate arrangement to distribute the flow, then the target average velocity
may be attained. The pressure drop found in the simulation is not difficult to achieve when
pumping a fluid such as water because it is fairly easy to pump liquids to high pressures.
Conclusion:
The final design is less than ideal but has the potential to lead to a much better solution to
the given design problem with some geometric modifications. The addition of more baffles will
result in a greater pressure drop but that should not be a problem because of how easy it is to
pump liquids to high pressures. In this case it may be a better idea to redesign the entire tank to
attain an even velocity profile along inspection line B.

More Related Content

What's hot

Analysis of Flow in a Convering-Diverging Nozzle
Analysis of Flow in a Convering-Diverging NozzleAnalysis of Flow in a Convering-Diverging Nozzle
Analysis of Flow in a Convering-Diverging NozzleAlber Douglawi
 
Streamline based history matching of arrival times and bottom-hole pressure d...
Streamline based history matching of arrival times and bottom-hole pressure d...Streamline based history matching of arrival times and bottom-hole pressure d...
Streamline based history matching of arrival times and bottom-hole pressure d...Shusei Tanaka
 
A novel approach for incorporation of capillary and gravity into streamline s...
A novel approach for incorporation of capillary and gravity into streamline s...A novel approach for incorporation of capillary and gravity into streamline s...
A novel approach for incorporation of capillary and gravity into streamline s...Shusei Tanaka
 
Thermodynamic optimization of
Thermodynamic optimization ofThermodynamic optimization of
Thermodynamic optimization ofJinoop AN
 
Determination of shock losses and pressure losses in ug mine openings
Determination of shock losses and pressure losses in ug mine openingsDetermination of shock losses and pressure losses in ug mine openings
Determination of shock losses and pressure losses in ug mine openingsSafdar Ali
 
Use of streamline flow diagnostics for injection production rate allocation o...
Use of streamline flow diagnostics for injection production rate allocation o...Use of streamline flow diagnostics for injection production rate allocation o...
Use of streamline flow diagnostics for injection production rate allocation o...Shusei Tanaka
 
Importance of mesh independence study
Importance of mesh independence studyImportance of mesh independence study
Importance of mesh independence studyChandra Prakash Lohia
 
Pros and-cons-of-cfd-and-physical-flow-modeling
Pros and-cons-of-cfd-and-physical-flow-modelingPros and-cons-of-cfd-and-physical-flow-modeling
Pros and-cons-of-cfd-and-physical-flow-modelingHashim Hasnain Hadi
 
CFD simulation and design optimization of heat exchanger purge manifold for m...
CFD simulation and design optimization of heat exchanger purge manifold for m...CFD simulation and design optimization of heat exchanger purge manifold for m...
CFD simulation and design optimization of heat exchanger purge manifold for m...Jan Rusås
 
AME-441-Group-47-Proposal-Approved
AME-441-Group-47-Proposal-ApprovedAME-441-Group-47-Proposal-Approved
AME-441-Group-47-Proposal-ApprovedAaron VanLandingham
 
Numerical simulation and optimization of high performance supersonic nozzle a...
Numerical simulation and optimization of high performance supersonic nozzle a...Numerical simulation and optimization of high performance supersonic nozzle a...
Numerical simulation and optimization of high performance supersonic nozzle a...eSAT Journals
 
Unconventional Data-Driven Methodologies Forecast Performance
Unconventional Data-Driven Methodologies Forecast PerformanceUnconventional Data-Driven Methodologies Forecast Performance
Unconventional Data-Driven Methodologies Forecast PerformanceKaanthan Shanmugam
 
Q921 re1 lec11 v1
Q921 re1 lec11 v1Q921 re1 lec11 v1
Q921 re1 lec11 v1AFATous
 
Study and analysis of convergent Divergent Nozzle Using CFD
Study and analysis of convergent Divergent Nozzle Using CFDStudy and analysis of convergent Divergent Nozzle Using CFD
Study and analysis of convergent Divergent Nozzle Using CFDAkhilendra Akki
 
CFD simulation of hrsg stack exhaust gas and its influence on nearby structu...
CFD simulation of hrsg stack exhaust gas and its influence on nearby  structu...CFD simulation of hrsg stack exhaust gas and its influence on nearby  structu...
CFD simulation of hrsg stack exhaust gas and its influence on nearby structu...Jan Rusås
 
An artificial intelligence based improved classification of two-phase flow patte...
An artificial intelligence based improved classification of two-phase flow patte...An artificial intelligence based improved classification of two-phase flow patte...
An artificial intelligence based improved classification of two-phase flow patte...ISA Interchange
 

What's hot (20)

Analysis of Flow in a Convering-Diverging Nozzle
Analysis of Flow in a Convering-Diverging NozzleAnalysis of Flow in a Convering-Diverging Nozzle
Analysis of Flow in a Convering-Diverging Nozzle
 
Streamline based history matching of arrival times and bottom-hole pressure d...
Streamline based history matching of arrival times and bottom-hole pressure d...Streamline based history matching of arrival times and bottom-hole pressure d...
Streamline based history matching of arrival times and bottom-hole pressure d...
 
A novel approach for incorporation of capillary and gravity into streamline s...
A novel approach for incorporation of capillary and gravity into streamline s...A novel approach for incorporation of capillary and gravity into streamline s...
A novel approach for incorporation of capillary and gravity into streamline s...
 
Master_Thesis_Koushik
Master_Thesis_KoushikMaster_Thesis_Koushik
Master_Thesis_Koushik
 
Thermodynamic optimization of
Thermodynamic optimization ofThermodynamic optimization of
Thermodynamic optimization of
 
Determination of shock losses and pressure losses in ug mine openings
Determination of shock losses and pressure losses in ug mine openingsDetermination of shock losses and pressure losses in ug mine openings
Determination of shock losses and pressure losses in ug mine openings
 
Use of streamline flow diagnostics for injection production rate allocation o...
Use of streamline flow diagnostics for injection production rate allocation o...Use of streamline flow diagnostics for injection production rate allocation o...
Use of streamline flow diagnostics for injection production rate allocation o...
 
ADP Project
ADP ProjectADP Project
ADP Project
 
Importance of mesh independence study
Importance of mesh independence studyImportance of mesh independence study
Importance of mesh independence study
 
Thesis presentation
Thesis presentationThesis presentation
Thesis presentation
 
Pros and-cons-of-cfd-and-physical-flow-modeling
Pros and-cons-of-cfd-and-physical-flow-modelingPros and-cons-of-cfd-and-physical-flow-modeling
Pros and-cons-of-cfd-and-physical-flow-modeling
 
CFD simulation and design optimization of heat exchanger purge manifold for m...
CFD simulation and design optimization of heat exchanger purge manifold for m...CFD simulation and design optimization of heat exchanger purge manifold for m...
CFD simulation and design optimization of heat exchanger purge manifold for m...
 
AME-441-Group-47-Proposal-Approved
AME-441-Group-47-Proposal-ApprovedAME-441-Group-47-Proposal-Approved
AME-441-Group-47-Proposal-Approved
 
Numerical simulation and optimization of high performance supersonic nozzle a...
Numerical simulation and optimization of high performance supersonic nozzle a...Numerical simulation and optimization of high performance supersonic nozzle a...
Numerical simulation and optimization of high performance supersonic nozzle a...
 
Unconventional Data-Driven Methodologies Forecast Performance
Unconventional Data-Driven Methodologies Forecast PerformanceUnconventional Data-Driven Methodologies Forecast Performance
Unconventional Data-Driven Methodologies Forecast Performance
 
Q921 re1 lec11 v1
Q921 re1 lec11 v1Q921 re1 lec11 v1
Q921 re1 lec11 v1
 
Study and analysis of convergent Divergent Nozzle Using CFD
Study and analysis of convergent Divergent Nozzle Using CFDStudy and analysis of convergent Divergent Nozzle Using CFD
Study and analysis of convergent Divergent Nozzle Using CFD
 
G1054048
G1054048G1054048
G1054048
 
CFD simulation of hrsg stack exhaust gas and its influence on nearby structu...
CFD simulation of hrsg stack exhaust gas and its influence on nearby  structu...CFD simulation of hrsg stack exhaust gas and its influence on nearby  structu...
CFD simulation of hrsg stack exhaust gas and its influence on nearby structu...
 
An artificial intelligence based improved classification of two-phase flow patte...
An artificial intelligence based improved classification of two-phase flow patte...An artificial intelligence based improved classification of two-phase flow patte...
An artificial intelligence based improved classification of two-phase flow patte...
 

Viewers also liked

Viewers also liked (14)

Design Portfolio-Hyewon Park
Design Portfolio-Hyewon ParkDesign Portfolio-Hyewon Park
Design Portfolio-Hyewon Park
 
Analisis Poster Film
Analisis Poster FilmAnalisis Poster Film
Analisis Poster Film
 
Peak1\'s Features
Peak1\'s FeaturesPeak1\'s Features
Peak1\'s Features
 
Trapezoide
TrapezoideTrapezoide
Trapezoide
 
Presentation1
Presentation1Presentation1
Presentation1
 
Practica
PracticaPractica
Practica
 
Mobile Development Presentation
Mobile Development PresentationMobile Development Presentation
Mobile Development Presentation
 
Cách chăm sóc đất baby chưa mở mắt
Cách chăm sóc đất baby chưa mở mắtCách chăm sóc đất baby chưa mở mắt
Cách chăm sóc đất baby chưa mở mắt
 
Practica
PracticaPractica
Practica
 
Аналитика и метрики моб приложений
Аналитика и метрики моб приложенийАналитика и метрики моб приложений
Аналитика и метрики моб приложений
 
Content Strategist's Guide to Design
Content Strategist's Guide to DesignContent Strategist's Guide to Design
Content Strategist's Guide to Design
 
Publicidadyrecursosliterarios 110321135520-phpapp01
Publicidadyrecursosliterarios 110321135520-phpapp01Publicidadyrecursosliterarios 110321135520-phpapp01
Publicidadyrecursosliterarios 110321135520-phpapp01
 
Presentation1
Presentation1Presentation1
Presentation1
 
Terminkalender
TerminkalenderTerminkalender
Terminkalender
 

Similar to Project 2 ME 4J03

Air flow and charge motion study of engine intake port
Air flow and charge motion study of engine intake portAir flow and charge motion study of engine intake port
Air flow and charge motion study of engine intake portTunAnh309
 
Case studies in cfd analysis by kk parthiban
Case studies in cfd analysis by kk parthibanCase studies in cfd analysis by kk parthiban
Case studies in cfd analysis by kk parthibanparthi2006
 
Server room cooling report
Server room cooling reportServer room cooling report
Server room cooling reportommuruga ps
 
conference paper
conference paperconference paper
conference paperRob Rosier
 
Application-Of-Laplace-Transform-To-Pressure-Transient-Analysis-In-A-Reservoi...
Application-Of-Laplace-Transform-To-Pressure-Transient-Analysis-In-A-Reservoi...Application-Of-Laplace-Transform-To-Pressure-Transient-Analysis-In-A-Reservoi...
Application-Of-Laplace-Transform-To-Pressure-Transient-Analysis-In-A-Reservoi...Oluwaseun Olaleye
 
Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...
Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...
Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...Dr. Amarjeet Singh
 
Determination of shock losses and pressure losses in ug mine openings (1)
Determination of shock losses and pressure losses in ug mine openings (1)Determination of shock losses and pressure losses in ug mine openings (1)
Determination of shock losses and pressure losses in ug mine openings (1)Safdar Ali
 
Performance Analysis of savonius hydro turbine using CFD simulation
Performance Analysis of savonius hydro turbine using CFD simulationPerformance Analysis of savonius hydro turbine using CFD simulation
Performance Analysis of savonius hydro turbine using CFD simulationIRJET Journal
 
An efficient algorithm for ogee spillway discharge with partiallyopened radia...
An efficient algorithm for ogee spillway discharge with partiallyopened radia...An efficient algorithm for ogee spillway discharge with partiallyopened radia...
An efficient algorithm for ogee spillway discharge with partiallyopened radia...theijes
 
Simplifying stormwater design is costing us money - a short case study
Simplifying stormwater design is costing us money - a short case studySimplifying stormwater design is costing us money - a short case study
Simplifying stormwater design is costing us money - a short case studyAdam Berry
 
Dynamic future flare_design2020
Dynamic future flare_design2020Dynamic future flare_design2020
Dynamic future flare_design2020Armin Mn
 
Seepage through an earth dam
Seepage through an earth damSeepage through an earth dam
Seepage through an earth damMan Xp
 
Sizing of water piping system
Sizing of water piping systemSizing of water piping system
Sizing of water piping systemTajudeen Ibrahim
 
Case Study: Blast Furnace Gas Distribution
Case Study: Blast Furnace Gas DistributionCase Study: Blast Furnace Gas Distribution
Case Study: Blast Furnace Gas DistributionFlex Process
 

Similar to Project 2 ME 4J03 (20)

Project 1 ME 4J03
Project 1 ME 4J03Project 1 ME 4J03
Project 1 ME 4J03
 
Air flow and charge motion study of engine intake port
Air flow and charge motion study of engine intake portAir flow and charge motion study of engine intake port
Air flow and charge motion study of engine intake port
 
Case studies in cfd analysis by kk parthiban
Case studies in cfd analysis by kk parthibanCase studies in cfd analysis by kk parthiban
Case studies in cfd analysis by kk parthiban
 
ASSIGNMENT
ASSIGNMENTASSIGNMENT
ASSIGNMENT
 
Server room cooling report
Server room cooling reportServer room cooling report
Server room cooling report
 
conference paper
conference paperconference paper
conference paper
 
Application-Of-Laplace-Transform-To-Pressure-Transient-Analysis-In-A-Reservoi...
Application-Of-Laplace-Transform-To-Pressure-Transient-Analysis-In-A-Reservoi...Application-Of-Laplace-Transform-To-Pressure-Transient-Analysis-In-A-Reservoi...
Application-Of-Laplace-Transform-To-Pressure-Transient-Analysis-In-A-Reservoi...
 
poster-Ash
poster-Ashposter-Ash
poster-Ash
 
Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...
Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...
Optimization of Closure Law of Guide Vanes for an Operational Hydropower Plan...
 
Determination of shock losses and pressure losses in ug mine openings (1)
Determination of shock losses and pressure losses in ug mine openings (1)Determination of shock losses and pressure losses in ug mine openings (1)
Determination of shock losses and pressure losses in ug mine openings (1)
 
Performance Analysis of savonius hydro turbine using CFD simulation
Performance Analysis of savonius hydro turbine using CFD simulationPerformance Analysis of savonius hydro turbine using CFD simulation
Performance Analysis of savonius hydro turbine using CFD simulation
 
An efficient algorithm for ogee spillway discharge with partiallyopened radia...
An efficient algorithm for ogee spillway discharge with partiallyopened radia...An efficient algorithm for ogee spillway discharge with partiallyopened radia...
An efficient algorithm for ogee spillway discharge with partiallyopened radia...
 
Simplifying stormwater design is costing us money - a short case study
Simplifying stormwater design is costing us money - a short case studySimplifying stormwater design is costing us money - a short case study
Simplifying stormwater design is costing us money - a short case study
 
Dynamic future flare_design2020
Dynamic future flare_design2020Dynamic future flare_design2020
Dynamic future flare_design2020
 
Problema 4
Problema 4Problema 4
Problema 4
 
Pump sizing basics
Pump sizing basicsPump sizing basics
Pump sizing basics
 
Seepage through an earth dam
Seepage through an earth damSeepage through an earth dam
Seepage through an earth dam
 
Sizing of water piping system
Sizing of water piping systemSizing of water piping system
Sizing of water piping system
 
Case Study: Blast Furnace Gas Distribution
Case Study: Blast Furnace Gas DistributionCase Study: Blast Furnace Gas Distribution
Case Study: Blast Furnace Gas Distribution
 
Pump efficiency
Pump efficiencyPump efficiency
Pump efficiency
 

Project 2 ME 4J03

  • 1. Mechanical Engineering 4J03 McMaster University Project #2 Prepared For: Dr. Hamed Date of Tutorial: March 6, 2015 Assignment Due Date: March 20, 2015 Prepared By: Shaun Chiasson, 1070043
  • 2. Objective: A cooling tank was to be examined for flow characteristics and pressure drop in order to determine a means to stabilize the water velocity that passes the cooling chamber. A design needed to be created that could bring the velocity at the chamber to a steady value within specified values while having an unlimited pressure allowance. The final design was to include the use of baffles and not change the tank in anyway. Results: From the given information in the problem the inlet velocity calculated was 0.673 m/s. The initial grid size indicated was too small to work with so a grid ten times larger was used. The original grid called for a 0.0007m mesh but instead a 0.007m mesh was used instead in order to save computation time. ( ) ( ) Figure 1: Flow velocity vector plot for the case of no baffles installed.
  • 3. Figure 2: Graph of velocity magnitudes for inspection lines A, B, and C for the case of no baffles installed. Figure 3: Graph of pressure magnitudes for inspection lines A, and C for the case of no baffles installed.
  • 4. Figure 4: First two attempts at a suitable baffle design. Figure 5: Second set of two attempts at a suitable baffle design.
  • 5. Figure 6: Third set of two attempts at a suitable baffle design. Figure 6: Fourth set of two attempts at a suitable baffle design.
  • 6. Figure 7: Fifth set of two attempts at a suitable baffle design. Figure 8: Final baffle design velocity vector plot.
  • 7. It is important to note that none of the designs tested would converge to the prescribed 1.0E-5 residual within the recommended three hundred iterations. Some designs did converge to the standard residual of 1.0E-4 but did not meet the requirements of the project. There was also sinusoidal variance in the residuals but not sufficient time to use double precision. Since none of the solutions are sufficient to meet the requirements and convergence was not met a grid independence test was not necessary. The final design presented here could meet the criteria with more work on the proposed geometry and may converge to 1.0E-5 if more iterations were allowed to run. The solution presented here has been resolved sufficiently well to conclude that the design can be reworked into a successful configuration because the mesh had been refined in the areas of the baffles where the gradients are highest as shown in Figure 9. Figure 9: Final baffle design mesh used in the solver.
  • 8. Figure 10: Graph of velocity magnitude for inspection line B for the final design. Figure 11: Graph of pressure magnitudes for inspection lines A, and C for the final design.
  • 9. Figure 12: Dimensions for the geometry of the final baffle design configuration. Note: Only the minimum amounts of dimensions are shown and those not shown can be assumed to be the same as others that are of the same magnitude and shown in the figure above. Discussion: The criterion for the velocity of the water states that an average of 80 fpm with a range of plus or minus ten percent would be desirable. To interpret the graphs above these values needed to be converted to meters per second. ( ) ( ) ( ) ( ) ( ) Figure 10 illustrates that a portion of the velocity magnitude graph lies within the range specified. This portion of the graph is fairly close to the edge of the cooling chamber circle, and this is the main reason to believe that with some minor alterations the final design could be made
  • 10. to satisfy the design criteria. The average velocity over the whole inspection line B will now be calculated from the graphs and compared to that of the case with no baffles installed. ̅ ( ) ̅ ( ) ̅ ̅ ̅ ( ) ( ) ( ) The addition of the baffle system has had a big impact on the average velocity of the water passing by inspection line B. This is the desired effect since the water initially enters the tank at a velocity of 0.673 m/s it is necessary to try and slow it down a great deal in order to attempt to reach the target velocity of 0.41 m/s. The addition of the baffles comes at a price however; the pressure drop in the tank has increased and will now be examined. ( ) The calculations above indicate that for relatively small decreases in the average velocity of the water a very large pressure drop will be required. This could mean that if more baffles are inserted in an appropriate arrangement to distribute the flow, then the target average velocity may be attained. The pressure drop found in the simulation is not difficult to achieve when pumping a fluid such as water because it is fairly easy to pump liquids to high pressures. Conclusion: The final design is less than ideal but has the potential to lead to a much better solution to the given design problem with some geometric modifications. The addition of more baffles will result in a greater pressure drop but that should not be a problem because of how easy it is to pump liquids to high pressures. In this case it may be a better idea to redesign the entire tank to attain an even velocity profile along inspection line B.