SlideShare une entreprise Scribd logo
1  sur  8
Télécharger pour lire hors ligne
CAD Design Portfolio
KOK WEE SOON
ABSTRACT
The document will cover the two major CAD/ Simulation projects
undertaken in the final year of university of which comprises the
Beyond Zero Emissions Melbourne CBD Wind Turbine project,
Race Car Front Wing Design and Simulation competition, and also
smaller projects undertaken previously.
2
Beyond Zero Emissions Melbourne
CBD Wind Turbine Project (2011)
This project focuses on the use of previously constructed CAD model of the
Melbourne CBD to run a wind simulation to identify possible viable spots on
rooftops to install wind turbines for green power generation. Due to the
complexity of the previous Autocad CAD models received, we were given
instructions as a team to construct the models in Gambit from scratch to clean
up the lines of which would lead to ease in future meshing for Computational
Fluid Dynamics (CFD) simulations.
The whole Melbourne CBD CAD model was split into various blocks of which
were assigned to each team member. This is then constructed again with the
Gambit software but measuring the pre-existing dimensions of the building
models provided. Samples of the constructed blocks can be seen as below in
Figure 1.
Figure 1: Google Maps (above) and Pre-existing AutoCAD model (below) of the Melbourne
CBD
3
Each block is individually modelled to approximated heights obtained from the
AutoCAD model in the Gambit modelling environment for compatibility with
the CFD program of which will be used at a later date to simulate fluid flow
over the compiled blocks. I was made in charge of modelling blocks B13_14,
B27_28, B29_30 and B33_34.
Due to Gambit being a relatively new operating environment for me
personally, I had to put in the effort to seek online tutorials to operate the
software and towards the end I was able to competently manage the
modelling of the city blocks as shown below in Figure 2.
Figure 2: Gambit modelling of individually delegated blocks of Melbourne CBD
4
The completed blocks are then compiled from all the team members for
further processing in Figure 3. The model has been passed on to the next
batch of volunteer engineers to pass it through CFD programs and ultimately
contribute to the study of viability of wind turbines in the CBD areas.
Figure 3: Compiled Melbourne CBD blocks as modelled by all team members
5
Race Car Front Wing Design
Project (2010)
This is one of the major projects undertaken during the 3rd
year of university
and involved the CAD design of a racecar front wing based on given
specifications and constraints. The Unigraphics NX7 CAD model is then
imported into ANSYS CFD and FEA module for simulation at given loads.
At the start of the project, we were required to construct an NX7 CAD model
from scratch based on the information provided. With the construction of the
model, variables are assigned to the inserted constraints to simplify future
changes to the model.
Figure 4: Variables as needed to design and adjust dimensions according to specifications
After the initial aerofoil model is constructed, end plates were added to the
design to reduce wingtip vortices from forming during simulation that would
contribute to a reduction in downforce generated as shown below. The model
shows a rib and spar construction of the wing.
Figure 5: Initial aerofoil constructed based on rib and spar internal construction
6
The designed wing, together with the car body and mounts, are imported into
ANSYS CFD and FEA modules to undergo simulations to check integrity and
performance of the wing. With the use of CFD, flow speeds and pressures
can be estimated with different wing designs, leading to a more efficient and
cost effective design of the wing. Downforce and drag coefficients on the wing
can be calculated and tabulated to generate a graph to select the best
designs.
Figure 6: ANSYS CFD Simulation of designed front wing and head
7
With Finite Element Analysis (FEA) of the wing when subjected to operating
loads, the stress, strain and deflection of the element can be seen at various
points of the structure. This is an important step to check the integrity of the
design when subjected to loads with the inclusion of the appropriate safety
factors.
Figure 7: ANSYS FEA Structural testing of front wing
By working as a team, we were able come in 4th
out of 22 teams competing.
This project has enabled us to be competent in using Unigraphics NX7 as a
means of engineering modelling and also ANSYS for simulation of the models
to verify the integrity of the designs produced.
8
Additional Projects
• Design of a Materials Impact Test Rig using Unigraphics NX7
(2009)
o CAD design work focusing on integrity of designed components
o Assembly with individually designed parts in the “ASSEMBLY”
mode into a final product
o Focused on the assembly constraint functions to limit the range
of motions of the components relative to each other
o Stress and strain on the components are calculated manually in
Excel
o Introduction to integration of variables into design for
streamlined change of specifications where applicable.
• Design of specimen holder for the Far-Infrared Beamline of the
Australian Synchrotron (2011)
o Designed a current specimen holder for spectroscopy machinery
with a higher aperture to allow higher transmitivity of far-infrared
x-rays (F-IR) from the beamline
o Drafted a CAD model of the holder to be passed onto the
mechanical workshop to be fabricated and PVD coated

Contenu connexe

Tendances

Fatigue Analysis of a Pressurized Aircraft Fuselage Modification using Hyperw...
Fatigue Analysis of a Pressurized Aircraft Fuselage Modification using Hyperw...Fatigue Analysis of a Pressurized Aircraft Fuselage Modification using Hyperw...
Fatigue Analysis of a Pressurized Aircraft Fuselage Modification using Hyperw...Altair
 
Drilling grid Alternative with 3D Printing
Drilling grid Alternative with 3D PrintingDrilling grid Alternative with 3D Printing
Drilling grid Alternative with 3D PrintingAltair
 
Mbd 06 kinematic-&_structural_simulation_of_the_automated_infotech
Mbd 06 kinematic-&_structural_simulation_of_the_automated_infotechMbd 06 kinematic-&_structural_simulation_of_the_automated_infotech
Mbd 06 kinematic-&_structural_simulation_of_the_automated_infotechAnand Kumar Chinni
 
Unit 2-ME8691 & COMPUTER AIDED DESIGN AND MANUFACTURING
Unit 2-ME8691 & COMPUTER AIDED DESIGN AND    MANUFACTURINGUnit 2-ME8691 & COMPUTER AIDED DESIGN AND    MANUFACTURING
Unit 2-ME8691 & COMPUTER AIDED DESIGN AND MANUFACTURINGMohanumar S
 
MEP Engineers on the way - How to improve MEP modeling with Dynamo
MEP Engineers on the way - How to improve MEP modeling with DynamoMEP Engineers on the way - How to improve MEP modeling with Dynamo
MEP Engineers on the way - How to improve MEP modeling with DynamoCesare Caoduro
 
Exploring the capabilities of the tight integration of HyperWorks and ESAComp
Exploring the capabilities of the tight integration of HyperWorks and ESACompExploring the capabilities of the tight integration of HyperWorks and ESAComp
Exploring the capabilities of the tight integration of HyperWorks and ESACompAltair
 
Romain AVY CV 2016
Romain AVY CV 2016Romain AVY CV 2016
Romain AVY CV 2016Romain Avy
 
ISC-2007-HPC-in-Aerodynamics-at-BMW-Norbert-Gruen
ISC-2007-HPC-in-Aerodynamics-at-BMW-Norbert-GruenISC-2007-HPC-in-Aerodynamics-at-BMW-Norbert-Gruen
ISC-2007-HPC-in-Aerodynamics-at-BMW-Norbert-GruenNorbert Gruen
 
INTRODUCTION TO COMPUTER AIDED DESIGN & MANUFACTURING
INTRODUCTION TO COMPUTER AIDED DESIGN & MANUFACTURINGINTRODUCTION TO COMPUTER AIDED DESIGN & MANUFACTURING
INTRODUCTION TO COMPUTER AIDED DESIGN & MANUFACTURINGBalamurugan Subburaj
 
Assessing the Aerodynamic Performance of a Formula SAE Model by means of CFD ...
Assessing the Aerodynamic Performance of a Formula SAE Model by means of CFD ...Assessing the Aerodynamic Performance of a Formula SAE Model by means of CFD ...
Assessing the Aerodynamic Performance of a Formula SAE Model by means of CFD ...saeid ghaffari
 
Design of Rear wing for high performance cars and Simulation using Computatio...
Design of Rear wing for high performance cars and Simulation using Computatio...Design of Rear wing for high performance cars and Simulation using Computatio...
Design of Rear wing for high performance cars and Simulation using Computatio...IJTET Journal
 
Drag Reduction of Front Wing of an F1 Car using Adjoint Optimisation
Drag Reduction of Front Wing of an F1 Car using Adjoint OptimisationDrag Reduction of Front Wing of an F1 Car using Adjoint Optimisation
Drag Reduction of Front Wing of an F1 Car using Adjoint Optimisationyasirmaliq
 
Surrogate Model-Based Reliability Analysis of Composite UAV Wing facilitation...
Surrogate Model-Based Reliability Analysis of Composite UAV Wing facilitation...Surrogate Model-Based Reliability Analysis of Composite UAV Wing facilitation...
Surrogate Model-Based Reliability Analysis of Composite UAV Wing facilitation...Altair
 
Aircraft Finite Element Modelling for structure analysis using Altair Products
Aircraft Finite Element Modelling for structure analysis using Altair ProductsAircraft Finite Element Modelling for structure analysis using Altair Products
Aircraft Finite Element Modelling for structure analysis using Altair ProductsAltair
 
Design and Analysis of Building using Etabs
Design and Analysis of Building using EtabsDesign and Analysis of Building using Etabs
Design and Analysis of Building using Etabsvishal shinde
 
IRJET- Flow Simulation for Aircraft using Computational Fluid Dynamics
IRJET- Flow Simulation for Aircraft using Computational Fluid DynamicsIRJET- Flow Simulation for Aircraft using Computational Fluid Dynamics
IRJET- Flow Simulation for Aircraft using Computational Fluid DynamicsIRJET Journal
 
New HyperWorks Pedestrian Impact Tool for vehicle engineering and CAE simulation
New HyperWorks Pedestrian Impact Tool for vehicle engineering and CAE simulationNew HyperWorks Pedestrian Impact Tool for vehicle engineering and CAE simulation
New HyperWorks Pedestrian Impact Tool for vehicle engineering and CAE simulationAltair
 

Tendances (20)

Fatigue Analysis of a Pressurized Aircraft Fuselage Modification using Hyperw...
Fatigue Analysis of a Pressurized Aircraft Fuselage Modification using Hyperw...Fatigue Analysis of a Pressurized Aircraft Fuselage Modification using Hyperw...
Fatigue Analysis of a Pressurized Aircraft Fuselage Modification using Hyperw...
 
Drilling grid Alternative with 3D Printing
Drilling grid Alternative with 3D PrintingDrilling grid Alternative with 3D Printing
Drilling grid Alternative with 3D Printing
 
Presentation_JeepCar
Presentation_JeepCarPresentation_JeepCar
Presentation_JeepCar
 
Mbd 06 kinematic-&_structural_simulation_of_the_automated_infotech
Mbd 06 kinematic-&_structural_simulation_of_the_automated_infotechMbd 06 kinematic-&_structural_simulation_of_the_automated_infotech
Mbd 06 kinematic-&_structural_simulation_of_the_automated_infotech
 
defense_PPT
defense_PPTdefense_PPT
defense_PPT
 
Unit 2-ME8691 & COMPUTER AIDED DESIGN AND MANUFACTURING
Unit 2-ME8691 & COMPUTER AIDED DESIGN AND    MANUFACTURINGUnit 2-ME8691 & COMPUTER AIDED DESIGN AND    MANUFACTURING
Unit 2-ME8691 & COMPUTER AIDED DESIGN AND MANUFACTURING
 
MEP Engineers on the way - How to improve MEP modeling with Dynamo
MEP Engineers on the way - How to improve MEP modeling with DynamoMEP Engineers on the way - How to improve MEP modeling with Dynamo
MEP Engineers on the way - How to improve MEP modeling with Dynamo
 
Exploring the capabilities of the tight integration of HyperWorks and ESAComp
Exploring the capabilities of the tight integration of HyperWorks and ESACompExploring the capabilities of the tight integration of HyperWorks and ESAComp
Exploring the capabilities of the tight integration of HyperWorks and ESAComp
 
Romain AVY CV 2016
Romain AVY CV 2016Romain AVY CV 2016
Romain AVY CV 2016
 
ISC-2007-HPC-in-Aerodynamics-at-BMW-Norbert-Gruen
ISC-2007-HPC-in-Aerodynamics-at-BMW-Norbert-GruenISC-2007-HPC-in-Aerodynamics-at-BMW-Norbert-Gruen
ISC-2007-HPC-in-Aerodynamics-at-BMW-Norbert-Gruen
 
INTRODUCTION TO COMPUTER AIDED DESIGN & MANUFACTURING
INTRODUCTION TO COMPUTER AIDED DESIGN & MANUFACTURINGINTRODUCTION TO COMPUTER AIDED DESIGN & MANUFACTURING
INTRODUCTION TO COMPUTER AIDED DESIGN & MANUFACTURING
 
Dissertation Poster
Dissertation PosterDissertation Poster
Dissertation Poster
 
Assessing the Aerodynamic Performance of a Formula SAE Model by means of CFD ...
Assessing the Aerodynamic Performance of a Formula SAE Model by means of CFD ...Assessing the Aerodynamic Performance of a Formula SAE Model by means of CFD ...
Assessing the Aerodynamic Performance of a Formula SAE Model by means of CFD ...
 
Design of Rear wing for high performance cars and Simulation using Computatio...
Design of Rear wing for high performance cars and Simulation using Computatio...Design of Rear wing for high performance cars and Simulation using Computatio...
Design of Rear wing for high performance cars and Simulation using Computatio...
 
Drag Reduction of Front Wing of an F1 Car using Adjoint Optimisation
Drag Reduction of Front Wing of an F1 Car using Adjoint OptimisationDrag Reduction of Front Wing of an F1 Car using Adjoint Optimisation
Drag Reduction of Front Wing of an F1 Car using Adjoint Optimisation
 
Surrogate Model-Based Reliability Analysis of Composite UAV Wing facilitation...
Surrogate Model-Based Reliability Analysis of Composite UAV Wing facilitation...Surrogate Model-Based Reliability Analysis of Composite UAV Wing facilitation...
Surrogate Model-Based Reliability Analysis of Composite UAV Wing facilitation...
 
Aircraft Finite Element Modelling for structure analysis using Altair Products
Aircraft Finite Element Modelling for structure analysis using Altair ProductsAircraft Finite Element Modelling for structure analysis using Altair Products
Aircraft Finite Element Modelling for structure analysis using Altair Products
 
Design and Analysis of Building using Etabs
Design and Analysis of Building using EtabsDesign and Analysis of Building using Etabs
Design and Analysis of Building using Etabs
 
IRJET- Flow Simulation for Aircraft using Computational Fluid Dynamics
IRJET- Flow Simulation for Aircraft using Computational Fluid DynamicsIRJET- Flow Simulation for Aircraft using Computational Fluid Dynamics
IRJET- Flow Simulation for Aircraft using Computational Fluid Dynamics
 
New HyperWorks Pedestrian Impact Tool for vehicle engineering and CAE simulation
New HyperWorks Pedestrian Impact Tool for vehicle engineering and CAE simulationNew HyperWorks Pedestrian Impact Tool for vehicle engineering and CAE simulation
New HyperWorks Pedestrian Impact Tool for vehicle engineering and CAE simulation
 

En vedette

Voluntrme Introduction
Voluntrme IntroductionVoluntrme Introduction
Voluntrme Introductionvoluntrme
 
Drakkar J. - Social Media Portfolio
Drakkar J. - Social Media PortfolioDrakkar J. - Social Media Portfolio
Drakkar J. - Social Media PortfolioDrakkar Jones
 
Lessons From Marriage
Lessons From MarriageLessons From Marriage
Lessons From MarriageJake Gunnoe
 
Học cách sống hòa bình với bệnh khớp
Học cách sống hòa bình với bệnh khớpHọc cách sống hòa bình với bệnh khớp
Học cách sống hòa bình với bệnh khớpjoellen270
 
Common Core for ALL kids
Common Core for ALL kidsCommon Core for ALL kids
Common Core for ALL kidsSarah Kesty
 
Tellurian 2016 Corporate Diaries and Notebooks in Dubai, UAE
Tellurian 2016 Corporate Diaries and Notebooks in Dubai, UAETellurian 2016 Corporate Diaries and Notebooks in Dubai, UAE
Tellurian 2016 Corporate Diaries and Notebooks in Dubai, UAETellurian Book Production
 
Cẩn thận với thoái hóa đốt sống cổ
Cẩn thận với thoái hóa đốt sống cổCẩn thận với thoái hóa đốt sống cổ
Cẩn thận với thoái hóa đốt sống cổjoesph652
 

En vedette (10)

I'm designer!
I'm designer!I'm designer!
I'm designer!
 
Voluntrme Introduction
Voluntrme IntroductionVoluntrme Introduction
Voluntrme Introduction
 
Drakkar J. - Social Media Portfolio
Drakkar J. - Social Media PortfolioDrakkar J. - Social Media Portfolio
Drakkar J. - Social Media Portfolio
 
fagu Resume final
fagu Resume finalfagu Resume final
fagu Resume final
 
Lessons From Marriage
Lessons From MarriageLessons From Marriage
Lessons From Marriage
 
Học cách sống hòa bình với bệnh khớp
Học cách sống hòa bình với bệnh khớpHọc cách sống hòa bình với bệnh khớp
Học cách sống hòa bình với bệnh khớp
 
Teeneger
TeenegerTeeneger
Teeneger
 
Common Core for ALL kids
Common Core for ALL kidsCommon Core for ALL kids
Common Core for ALL kids
 
Tellurian 2016 Corporate Diaries and Notebooks in Dubai, UAE
Tellurian 2016 Corporate Diaries and Notebooks in Dubai, UAETellurian 2016 Corporate Diaries and Notebooks in Dubai, UAE
Tellurian 2016 Corporate Diaries and Notebooks in Dubai, UAE
 
Cẩn thận với thoái hóa đốt sống cổ
Cẩn thận với thoái hóa đốt sống cổCẩn thận với thoái hóa đốt sống cổ
Cẩn thận với thoái hóa đốt sống cổ
 

Similaire à KW_SOON_CAD_DESIGN_PORTFOLIO

Dd3210971099
Dd3210971099Dd3210971099
Dd3210971099IJMER
 
CFD Analysis of conceptual Aircraft body
CFD Analysis of conceptual Aircraft bodyCFD Analysis of conceptual Aircraft body
CFD Analysis of conceptual Aircraft bodyIRJET Journal
 
IRJET-CFD Analysis of conceptual Aircraft body
IRJET-CFD Analysis of conceptual Aircraft bodyIRJET-CFD Analysis of conceptual Aircraft body
IRJET-CFD Analysis of conceptual Aircraft bodyIRJET Journal
 
Ardent CATIA Project - Boeing 787.docx
Ardent CATIA Project - Boeing 787.docxArdent CATIA Project - Boeing 787.docx
Ardent CATIA Project - Boeing 787.docxSKMOBASSARULHAQUE
 
International Journal of Engineering Research and Development
International Journal of Engineering Research and Development International Journal of Engineering Research and Development
International Journal of Engineering Research and Development IJERD Editor
 
Development_of_Computer_Aided_Critical_Lift_Planning_Software-libre
Development_of_Computer_Aided_Critical_Lift_Planning_Software-libreDevelopment_of_Computer_Aided_Critical_Lift_Planning_Software-libre
Development_of_Computer_Aided_Critical_Lift_Planning_Software-libreSrikanth Chadalavada
 
CURRICULUM VITAE_Balu
CURRICULUM VITAE_BaluCURRICULUM VITAE_Balu
CURRICULUM VITAE_Balubalakrishna H
 
IRJET-Multi-Material & Lightweight Design Optimization of a Volvo B9r Bus Fra...
IRJET-Multi-Material & Lightweight Design Optimization of a Volvo B9r Bus Fra...IRJET-Multi-Material & Lightweight Design Optimization of a Volvo B9r Bus Fra...
IRJET-Multi-Material & Lightweight Design Optimization of a Volvo B9r Bus Fra...IRJET Journal
 
CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...
CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...
CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...IOSR Journals
 
Computational steering Interactive Design-through-Analysis for Simulation Sci...
Computational steering Interactive Design-through-Analysis for Simulation Sci...Computational steering Interactive Design-through-Analysis for Simulation Sci...
Computational steering Interactive Design-through-Analysis for Simulation Sci...SURFevents
 
How Accurate is Future Facilities 6Sigma DCX
How Accurate is Future Facilities 6Sigma DCXHow Accurate is Future Facilities 6Sigma DCX
How Accurate is Future Facilities 6Sigma DCXRobert Schmidt
 
IRJET- Design Automation of Cam Lobe Modeling in Creo using C#
IRJET- Design Automation of Cam Lobe Modeling in Creo using C#IRJET- Design Automation of Cam Lobe Modeling in Creo using C#
IRJET- Design Automation of Cam Lobe Modeling in Creo using C#IRJET Journal
 
Towards smart and sustainable machining
Towards smart and sustainable machiningTowards smart and sustainable machining
Towards smart and sustainable machiningLiu PeiLing
 

Similaire à KW_SOON_CAD_DESIGN_PORTFOLIO (20)

Portfolio_new
Portfolio_newPortfolio_new
Portfolio_new
 
Dd3210971099
Dd3210971099Dd3210971099
Dd3210971099
 
CFD Analysis of conceptual Aircraft body
CFD Analysis of conceptual Aircraft bodyCFD Analysis of conceptual Aircraft body
CFD Analysis of conceptual Aircraft body
 
IRJET-CFD Analysis of conceptual Aircraft body
IRJET-CFD Analysis of conceptual Aircraft bodyIRJET-CFD Analysis of conceptual Aircraft body
IRJET-CFD Analysis of conceptual Aircraft body
 
Ardent CATIA Project - Boeing 787.docx
Ardent CATIA Project - Boeing 787.docxArdent CATIA Project - Boeing 787.docx
Ardent CATIA Project - Boeing 787.docx
 
International Journal of Engineering Research and Development
International Journal of Engineering Research and Development International Journal of Engineering Research and Development
International Journal of Engineering Research and Development
 
Development_of_Computer_Aided_Critical_Lift_Planning_Software-libre
Development_of_Computer_Aided_Critical_Lift_Planning_Software-libreDevelopment_of_Computer_Aided_Critical_Lift_Planning_Software-libre
Development_of_Computer_Aided_Critical_Lift_Planning_Software-libre
 
Resume_Praveenkumar K Hiremath
Resume_Praveenkumar K HiremathResume_Praveenkumar K Hiremath
Resume_Praveenkumar K Hiremath
 
CURRICULUM VITAE_Balu
CURRICULUM VITAE_BaluCURRICULUM VITAE_Balu
CURRICULUM VITAE_Balu
 
IRJET-Multi-Material & Lightweight Design Optimization of a Volvo B9r Bus Fra...
IRJET-Multi-Material & Lightweight Design Optimization of a Volvo B9r Bus Fra...IRJET-Multi-Material & Lightweight Design Optimization of a Volvo B9r Bus Fra...
IRJET-Multi-Material & Lightweight Design Optimization of a Volvo B9r Bus Fra...
 
Basics of sap2000
Basics of sap2000 Basics of sap2000
Basics of sap2000
 
Krishankant Sharma Portfolio
Krishankant Sharma PortfolioKrishankant Sharma Portfolio
Krishankant Sharma Portfolio
 
CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...
CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...
CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...
 
Computational steering Interactive Design-through-Analysis for Simulation Sci...
Computational steering Interactive Design-through-Analysis for Simulation Sci...Computational steering Interactive Design-through-Analysis for Simulation Sci...
Computational steering Interactive Design-through-Analysis for Simulation Sci...
 
How Accurate is Future Facilities 6Sigma DCX
How Accurate is Future Facilities 6Sigma DCXHow Accurate is Future Facilities 6Sigma DCX
How Accurate is Future Facilities 6Sigma DCX
 
IRJET- Design Automation of Cam Lobe Modeling in Creo using C#
IRJET- Design Automation of Cam Lobe Modeling in Creo using C#IRJET- Design Automation of Cam Lobe Modeling in Creo using C#
IRJET- Design Automation of Cam Lobe Modeling in Creo using C#
 
Towards smart and sustainable machining
Towards smart and sustainable machiningTowards smart and sustainable machining
Towards smart and sustainable machining
 
Bmw
BmwBmw
Bmw
 
Cad Port 2
Cad Port 2Cad Port 2
Cad Port 2
 
Solidworks software
Solidworks softwareSolidworks software
Solidworks software
 

KW_SOON_CAD_DESIGN_PORTFOLIO

  • 1. CAD Design Portfolio KOK WEE SOON ABSTRACT The document will cover the two major CAD/ Simulation projects undertaken in the final year of university of which comprises the Beyond Zero Emissions Melbourne CBD Wind Turbine project, Race Car Front Wing Design and Simulation competition, and also smaller projects undertaken previously.
  • 2. 2 Beyond Zero Emissions Melbourne CBD Wind Turbine Project (2011) This project focuses on the use of previously constructed CAD model of the Melbourne CBD to run a wind simulation to identify possible viable spots on rooftops to install wind turbines for green power generation. Due to the complexity of the previous Autocad CAD models received, we were given instructions as a team to construct the models in Gambit from scratch to clean up the lines of which would lead to ease in future meshing for Computational Fluid Dynamics (CFD) simulations. The whole Melbourne CBD CAD model was split into various blocks of which were assigned to each team member. This is then constructed again with the Gambit software but measuring the pre-existing dimensions of the building models provided. Samples of the constructed blocks can be seen as below in Figure 1. Figure 1: Google Maps (above) and Pre-existing AutoCAD model (below) of the Melbourne CBD
  • 3. 3 Each block is individually modelled to approximated heights obtained from the AutoCAD model in the Gambit modelling environment for compatibility with the CFD program of which will be used at a later date to simulate fluid flow over the compiled blocks. I was made in charge of modelling blocks B13_14, B27_28, B29_30 and B33_34. Due to Gambit being a relatively new operating environment for me personally, I had to put in the effort to seek online tutorials to operate the software and towards the end I was able to competently manage the modelling of the city blocks as shown below in Figure 2. Figure 2: Gambit modelling of individually delegated blocks of Melbourne CBD
  • 4. 4 The completed blocks are then compiled from all the team members for further processing in Figure 3. The model has been passed on to the next batch of volunteer engineers to pass it through CFD programs and ultimately contribute to the study of viability of wind turbines in the CBD areas. Figure 3: Compiled Melbourne CBD blocks as modelled by all team members
  • 5. 5 Race Car Front Wing Design Project (2010) This is one of the major projects undertaken during the 3rd year of university and involved the CAD design of a racecar front wing based on given specifications and constraints. The Unigraphics NX7 CAD model is then imported into ANSYS CFD and FEA module for simulation at given loads. At the start of the project, we were required to construct an NX7 CAD model from scratch based on the information provided. With the construction of the model, variables are assigned to the inserted constraints to simplify future changes to the model. Figure 4: Variables as needed to design and adjust dimensions according to specifications After the initial aerofoil model is constructed, end plates were added to the design to reduce wingtip vortices from forming during simulation that would contribute to a reduction in downforce generated as shown below. The model shows a rib and spar construction of the wing. Figure 5: Initial aerofoil constructed based on rib and spar internal construction
  • 6. 6 The designed wing, together with the car body and mounts, are imported into ANSYS CFD and FEA modules to undergo simulations to check integrity and performance of the wing. With the use of CFD, flow speeds and pressures can be estimated with different wing designs, leading to a more efficient and cost effective design of the wing. Downforce and drag coefficients on the wing can be calculated and tabulated to generate a graph to select the best designs. Figure 6: ANSYS CFD Simulation of designed front wing and head
  • 7. 7 With Finite Element Analysis (FEA) of the wing when subjected to operating loads, the stress, strain and deflection of the element can be seen at various points of the structure. This is an important step to check the integrity of the design when subjected to loads with the inclusion of the appropriate safety factors. Figure 7: ANSYS FEA Structural testing of front wing By working as a team, we were able come in 4th out of 22 teams competing. This project has enabled us to be competent in using Unigraphics NX7 as a means of engineering modelling and also ANSYS for simulation of the models to verify the integrity of the designs produced.
  • 8. 8 Additional Projects • Design of a Materials Impact Test Rig using Unigraphics NX7 (2009) o CAD design work focusing on integrity of designed components o Assembly with individually designed parts in the “ASSEMBLY” mode into a final product o Focused on the assembly constraint functions to limit the range of motions of the components relative to each other o Stress and strain on the components are calculated manually in Excel o Introduction to integration of variables into design for streamlined change of specifications where applicable. • Design of specimen holder for the Far-Infrared Beamline of the Australian Synchrotron (2011) o Designed a current specimen holder for spectroscopy machinery with a higher aperture to allow higher transmitivity of far-infrared x-rays (F-IR) from the beamline o Drafted a CAD model of the holder to be passed onto the mechanical workshop to be fabricated and PVD coated