A presentation given at the SAE COMVEC conference this year during the CFD expert panel. Focuses on the new adjoint solver that is part of the automotive CFD suite, Elements, from Streamline Solutions.
CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...IOSR Journals
This work proposes an effective numerical model based on the Computational Fluid Dynamics
(CFD) approach to obtain the flow structure around a passenger car with Tail Plates. The experimental work of
the test vehicle and grid system is constructed by ANSYS-14.0. FLUENT which is the CFD solver & employed in
the present work. In this study, numerical iterations are completed, then after aerodynamic data and detailed
complicated flow structure are visualized.
In the present work, model of generic passenger car has been developed in solid works-10 and
generated the wind tunnel and applied the boundary conditions in ANSYS workbench 14.0 platform then after
testing and simulation has been performed for the evaluation of drag coefficient for passenger car. In another
case, the aerodynamics of the most suitable design of tail plate is introduced and analysedfor the evaluation of
drag coefficient for passenger car. The addition of tail plates results in a reduction of the drag-coefficient
3.87% and lift coefficient 16.62% in head-on wind. Rounding the edges partially reduces drag in head-on wind
but does not bring about the significant improvements in the aerodynamic efficiency of the passenger car with
tail plates, it can be obtained. Hence, the drag force can be reduced by using add on devices on vehicle and fuel
economy, stability of a passenger car can be improved.
Drag Reduction of Front Wing of an F1 Car using Adjoint Optimisationyasirmaliq
The Project Poster summarizes the aims and objectives of the Final Year Dissertation. The project starts with a detailed study on the parameters that tend to affect the performance of front wings of an F1 car and goes through designing the front wings(3) with endplates and wheel, meshing it, solving/analysing the flow and finally optimising the selected geometry using Fluent Adjoint Solver for efficient performance.
Adjoint optimisation technique is used to achieve optimal performance from the front wings. It's the most successful shape optimisation method as it's independent of the number of design variables exponentially reducing computational time and cost. The emphasis has been put on optimising the shape of the front wings using the Adjoint method as it’s the most efficient and computationally inexpensive method for design optimisation. The approach towards shape optimisation is downforce constrained drag minimization as it would result in keeping a constraint on downforce and reducing the drag at the same time, thus producing optima for a given downforce/drag value.
A presentation given at the SAE COMVEC conference this year during the CFD expert panel. Focuses on the new adjoint solver that is part of the automotive CFD suite, Elements, from Streamline Solutions.
CFD Simulation for Flow over Passenger Car Using Tail Plates for Aerodynamic ...IOSR Journals
This work proposes an effective numerical model based on the Computational Fluid Dynamics
(CFD) approach to obtain the flow structure around a passenger car with Tail Plates. The experimental work of
the test vehicle and grid system is constructed by ANSYS-14.0. FLUENT which is the CFD solver & employed in
the present work. In this study, numerical iterations are completed, then after aerodynamic data and detailed
complicated flow structure are visualized.
In the present work, model of generic passenger car has been developed in solid works-10 and
generated the wind tunnel and applied the boundary conditions in ANSYS workbench 14.0 platform then after
testing and simulation has been performed for the evaluation of drag coefficient for passenger car. In another
case, the aerodynamics of the most suitable design of tail plate is introduced and analysedfor the evaluation of
drag coefficient for passenger car. The addition of tail plates results in a reduction of the drag-coefficient
3.87% and lift coefficient 16.62% in head-on wind. Rounding the edges partially reduces drag in head-on wind
but does not bring about the significant improvements in the aerodynamic efficiency of the passenger car with
tail plates, it can be obtained. Hence, the drag force can be reduced by using add on devices on vehicle and fuel
economy, stability of a passenger car can be improved.
Drag Reduction of Front Wing of an F1 Car using Adjoint Optimisationyasirmaliq
The Project Poster summarizes the aims and objectives of the Final Year Dissertation. The project starts with a detailed study on the parameters that tend to affect the performance of front wings of an F1 car and goes through designing the front wings(3) with endplates and wheel, meshing it, solving/analysing the flow and finally optimising the selected geometry using Fluent Adjoint Solver for efficient performance.
Adjoint optimisation technique is used to achieve optimal performance from the front wings. It's the most successful shape optimisation method as it's independent of the number of design variables exponentially reducing computational time and cost. The emphasis has been put on optimising the shape of the front wings using the Adjoint method as it’s the most efficient and computationally inexpensive method for design optimisation. The approach towards shape optimisation is downforce constrained drag minimization as it would result in keeping a constraint on downforce and reducing the drag at the same time, thus producing optima for a given downforce/drag value.
SIMPACK - a high-end Multi-body simulation tool, gives you complete insight of Multi-body dynamics. There are quite a few users in India, of which we had a User Meet, to take the Users inputs and to understand their difficulties. User meet will be held every year to understand the progress of our customers. Want to know more about SIMPACK MBD or the solely authorized SIMPACK distributor, feel free to contact us.
Design of Rear wing for high performance cars and Simulation using Computatio...IJTET Journal
The performance of a sports car is not only limited to its engine power but also to aerodynamic properties of the car. By decreasing the drag force it is possible to reduce the engine power required to achieve same top speed thus decreasing the fuel requirement. The stability of a sports car is considerably important at high speed. The provision of a rear wing increases the downforce thus reducing the rear axle lift and provides increased traction. In this study an optimum rear wing is designed for the high performance car so as to decrease drag and increase downforce. The CAD designed baseline model with or without rear wing is being analyzed in computational fluid dynamics software. The lift and drag coefficient are calculated for all the design thus an optimum rear wing is designed for the considered baseline model.
Aircraft Finite Element Modelling for structure analysis using Altair ProductsAltair
The Airbus airframe design process has considerably evolved since 20 years with the constant improvement of numerical simulation capability and the computational means capacity. Today the size of Finite Element Models for aircraft structural behaviour study is exceeding the boundary of airframe components (fuselage section, wing); for the A350, a very large scale non-linear model of more than 60 million degrees of freedom has been developed to secure the static test campaign. This communication will illustrate the partnership with Altair and the use of Altair products for the creation and verification of very large models at Airbus. It will deal with: - Geometry preparation - Meshing - Property assignment - Assembly - Checking More generally, numerical simulation will play more and more a major role in the aircraft process, from the development of new concepts / derivatives to the support of the in-service fleet. Then, this presentation will also state the coming needs regarding model creation tools to cope with Airbus strategy.
Speakers
Marion Touboul, Ingénieur en Simulation Numérique - Calcul Structure, Airbus Opérations SAS
In this module, we will discuss different techniques for lane management and the method for feasibility assessment.
Lane Reversal
High Occupancy Vehicle (HOV) Lane
Shoulder Lane
International Journal of Engineering Research and Development IJERD Editor
• Electrical, Electronics and Computer Engineering,
• Information Engineering and Technology,
• Mechanical, Industrial and Manufacturing Engineering,
• Automation and Mechatronics Engineering,
• Material and Chemical Engineering,
• Civil and Architecture Engineering,
• Biotechnology and Bio Engineering,
• Environmental Engineering,
• Petroleum and Mining Engineering,
• Marine and Agriculture engineering,
• Aerospace Engineering.
SIMPACK - a high-end Multi-body simulation tool, gives you complete insight of Multi-body dynamics. There are quite a few users in India, of which we had a User Meet, to take the Users inputs and to understand their difficulties. User meet will be held every year to understand the progress of our customers. Want to know more about SIMPACK MBD or the solely authorized SIMPACK distributor, feel free to contact us.
Design of Rear wing for high performance cars and Simulation using Computatio...IJTET Journal
The performance of a sports car is not only limited to its engine power but also to aerodynamic properties of the car. By decreasing the drag force it is possible to reduce the engine power required to achieve same top speed thus decreasing the fuel requirement. The stability of a sports car is considerably important at high speed. The provision of a rear wing increases the downforce thus reducing the rear axle lift and provides increased traction. In this study an optimum rear wing is designed for the high performance car so as to decrease drag and increase downforce. The CAD designed baseline model with or without rear wing is being analyzed in computational fluid dynamics software. The lift and drag coefficient are calculated for all the design thus an optimum rear wing is designed for the considered baseline model.
Aircraft Finite Element Modelling for structure analysis using Altair ProductsAltair
The Airbus airframe design process has considerably evolved since 20 years with the constant improvement of numerical simulation capability and the computational means capacity. Today the size of Finite Element Models for aircraft structural behaviour study is exceeding the boundary of airframe components (fuselage section, wing); for the A350, a very large scale non-linear model of more than 60 million degrees of freedom has been developed to secure the static test campaign. This communication will illustrate the partnership with Altair and the use of Altair products for the creation and verification of very large models at Airbus. It will deal with: - Geometry preparation - Meshing - Property assignment - Assembly - Checking More generally, numerical simulation will play more and more a major role in the aircraft process, from the development of new concepts / derivatives to the support of the in-service fleet. Then, this presentation will also state the coming needs regarding model creation tools to cope with Airbus strategy.
Speakers
Marion Touboul, Ingénieur en Simulation Numérique - Calcul Structure, Airbus Opérations SAS
In this module, we will discuss different techniques for lane management and the method for feasibility assessment.
Lane Reversal
High Occupancy Vehicle (HOV) Lane
Shoulder Lane
International Journal of Engineering Research and Development IJERD Editor
• Electrical, Electronics and Computer Engineering,
• Information Engineering and Technology,
• Mechanical, Industrial and Manufacturing Engineering,
• Automation and Mechatronics Engineering,
• Material and Chemical Engineering,
• Civil and Architecture Engineering,
• Biotechnology and Bio Engineering,
• Environmental Engineering,
• Petroleum and Mining Engineering,
• Marine and Agriculture engineering,
• Aerospace Engineering.
JPRO Professional Heavy Duty Truck Diagnostic Toolbox User ManualTim Miller
This is the user manual of JPRO Professional Heavy Duty Truck Diagnostic Toolbox.
>> READ MORE: https://www.obdadvisor.com/autel-scanners/
Here is a detailed review of the toolbox based on my own experience, including:
- Compatibility
- Display
- Software
- Features and Functions
- Pros and Cons
Check it out to get the REVIEW and some NOTES about using this tool.
Evolution of Vehicle aftter it has been released, How its made and managedSamuel Festus
a research project based on the theme: Evolution of vehicle after it has been released, how it’s made, and how it’s managed.
Focusing on the Renault system design used in the manufacturing of Automotive and also Serial life management.
How China NCAP is promoting the progress of automotive technical development ...Global NCAP
How China NCAP is promoting the progress of automotive technical development in China. Presentation given at the 2014 Global NCAP Annual Meeting. CATARC, Tianjin, China. 30 October 2014
Teaching How to use the CFD Approach by an Example: Hydrodynamics within a Pa...Nelson García Polanco
The CDF methodology is applied to the study of the air flow around a 2-D car and its interaction with the cabin internal air. The flow visualization or computational works enable engineers to calculate different car characteristics like drag coefficient, external and internal air flow patterns.The results show the physics behavior of the flow and the presence of flow structures, as for instance, indoor air recirculation zones.
Tractor-trailers are used all across America to transport cargo, but are not designed with fuel efficiency in mind. Therefor, there is an incentive for companies to invest in making their tractor-trailers more aerodynamic in order to save on fuel costs. I go into the testing and methodology of how my team and I decided to tackle the problem of reducing the coefficient of drag on tractor-trailers by implementing air channeling devices (ACDs). Then, I cover the results from our experiments and our ACD recommendation.
Similar to NAFEMS Americas Elements presentation (20)
Online aptitude test management system project report.pdfKamal Acharya
The purpose of on-line aptitude test system is to take online test in an efficient manner and no time wasting for checking the paper. The main objective of on-line aptitude test system is to efficiently evaluate the candidate thoroughly through a fully automated system that not only saves lot of time but also gives fast results. For students they give papers according to their convenience and time and there is no need of using extra thing like paper, pen etc. This can be used in educational institutions as well as in corporate world. Can be used anywhere any time as it is a web based application (user Location doesn’t matter). No restriction that examiner has to be present when the candidate takes the test.
Every time when lecturers/professors need to conduct examinations they have to sit down think about the questions and then create a whole new set of questions for each and every exam. In some cases the professor may want to give an open book online exam that is the student can take the exam any time anywhere, but the student might have to answer the questions in a limited time period. The professor may want to change the sequence of questions for every student. The problem that a student has is whenever a date for the exam is declared the student has to take it and there is no way he can take it at some other time. This project will create an interface for the examiner to create and store questions in a repository. It will also create an interface for the student to take examinations at his convenience and the questions and/or exams may be timed. Thereby creating an application which can be used by examiners and examinee’s simultaneously.
Examination System is very useful for Teachers/Professors. As in the teaching profession, you are responsible for writing question papers. In the conventional method, you write the question paper on paper, keep question papers separate from answers and all this information you have to keep in a locker to avoid unauthorized access. Using the Examination System you can create a question paper and everything will be written to a single exam file in encrypted format. You can set the General and Administrator password to avoid unauthorized access to your question paper. Every time you start the examination, the program shuffles all the questions and selects them randomly from the database, which reduces the chances of memorizing the questions.
Cosmetic shop management system project report.pdfKamal Acharya
Buying new cosmetic products is difficult. It can even be scary for those who have sensitive skin and are prone to skin trouble. The information needed to alleviate this problem is on the back of each product, but it's thought to interpret those ingredient lists unless you have a background in chemistry.
Instead of buying and hoping for the best, we can use data science to help us predict which products may be good fits for us. It includes various function programs to do the above mentioned tasks.
Data file handling has been effectively used in the program.
The automated cosmetic shop management system should deal with the automation of general workflow and administration process of the shop. The main processes of the system focus on customer's request where the system is able to search the most appropriate products and deliver it to the customers. It should help the employees to quickly identify the list of cosmetic product that have reached the minimum quantity and also keep a track of expired date for each cosmetic product. It should help the employees to find the rack number in which the product is placed.It is also Faster and more efficient way.
Harnessing WebAssembly for Real-time Stateless Streaming PipelinesChristina Lin
Traditionally, dealing with real-time data pipelines has involved significant overhead, even for straightforward tasks like data transformation or masking. However, in this talk, we’ll venture into the dynamic realm of WebAssembly (WASM) and discover how it can revolutionize the creation of stateless streaming pipelines within a Kafka (Redpanda) broker. These pipelines are adept at managing low-latency, high-data-volume scenarios.
Using recycled concrete aggregates (RCA) for pavements is crucial to achieving sustainability. Implementing RCA for new pavement can minimize carbon footprint, conserve natural resources, reduce harmful emissions, and lower life cycle costs. Compared to natural aggregate (NA), RCA pavement has fewer comprehensive studies and sustainability assessments.
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...Dr.Costas Sachpazis
Terzaghi's soil bearing capacity theory, developed by Karl Terzaghi, is a fundamental principle in geotechnical engineering used to determine the bearing capacity of shallow foundations. This theory provides a method to calculate the ultimate bearing capacity of soil, which is the maximum load per unit area that the soil can support without undergoing shear failure. The Calculation HTML Code included.
Welcome to WIPAC Monthly the magazine brought to you by the LinkedIn Group Water Industry Process Automation & Control.
In this month's edition, along with this month's industry news to celebrate the 13 years since the group was created we have articles including
A case study of the used of Advanced Process Control at the Wastewater Treatment works at Lleida in Spain
A look back on an article on smart wastewater networks in order to see how the industry has measured up in the interim around the adoption of Digital Transformation in the Water Industry.
1. VALIDATION OF A NOVEL CAE
SOFTWARE SUITE AGAINST AN
EXTENSIVE DATA SET OF
AUTOMOTIVE AERODYNAMICS
TEST CASES
Angus Lock
Head of Aerodynamics
Auto Research Center
2. Streamline Solutions | Who We Are
AUTO RESEARCH CENTER
Automotive Engineering R&D, Wind
Tunnel, 7-Post & Gearbox Rig
ENGYS
CFD Engineering, MDO, Open Source
Software Development, User Support
STREAMLINE SOLUTIONS
Joint
Venture
www.arcindy.com www.engys.com
3. Streamline Solutions | Open Source
• Streamline Solutions
have built an end to
end open source CFD
process
• Scripting, geometry
clean-up and
creation, morphing,
meshing, solving,
optimization and post-
processing are all
conducted using open
source tools
7. CFD Modelling | Post-Processing
• Automated, batch driven co- and post-processing:
– Contour plots of U, p, tauw, Unw fields
– Isosurfaces of Ptot
– Averaged CD and CL, Cp
– Force development plots
– HTML / WEBGL reporting C:/Users/alock/Desktop/motorBike/test.html
9. Validation | Parametric Changes
• Fixed Ground
• 5-belt Moving Ground
• Single Belt Moving
Ground
• Yaw Angle
• Ride Height
• Test Speed
• Vehicle Modifications
(e.g. Open or Closed
Cooling, Spoiler on/off,
Underbody Panels on/off)
10. Validation | ARC Wind Tunnel
• Max Wind Speed : 50 m/s
• Max Road Speed: 50 m/s
• Nozzle Size: 2.3 m x 2.1 m
• Contraction Ratio: 4.8 : 1.0
• Moving Belt Size: 3.4 m x 1.7 m
• Boundary Layer Thickness: 1mm
• Main Fan Motor Power: 320 kW
• Primary BL Motor Power: 80 kW
• Secondary BL Motor Power: 19 kW
• Rolling Road Motor Power: 120 kW
Rapid prototyping, workshops &
office space
Moving ground, scale-model wind tunnel
Vehicle dynamics 7-post rig
11. Validation | Aerodynamic Balance
• Models are mounted in the tunnel by means of an overhead sting
• The 6-component balance is contained within the model
• Secondary balance for tractor-trailer
12. Validation | Instrumentation
• 128 pressure channels to allow for evaluation of surface
pressures from around the model
• Cooling mass-flow measurement by a grid of up to 14 vane type
anemometers
13. Validation | Flowfield Comparison
• Extensive work was
conducted to compare
flow field structure
• The figures below
illustrate the correlation
between the CFD
predictions and wind
tunnel data for the
DrivAer models (SAE
2012-01-1068)
13
14. Validation | Flowfield Comparison
14
Upper surfaces Lower surfaces
• Comparison of centerline pressures on fastback
15. Validation | Flowfield Comparison
15
Experiment CFD
• Comparison of surface pressures on fastback windshield
16. Validation | Flowfield Comparison
16
Experiment CFD
• Comparison of surface pressures on fastback windshield
17. Validation | Flowfield Comparison
17
Experiment CFD
• Comparison of surface pressures on fastback windshield
18. Validation | Flowfield Comparison
18
Experiment CFD
• Comparison of surface pressures on fastback windshield
19. Validation | Flowfield Comparison
19
Experiment CFD
• Comparison of surface pressures on fastback windshield
20. Validation | Results
CD CLF CLR
1 DRIVAER Estate n/a 40% SingleBelt 2.40%
2 DRIVAER Fast n/a 40% SingleBelt -0.41%
3 DRIVAER Notch n/a 40% SingleBelt 0.41%
4 Sedan 1 open 100% 5 Belt 0.67% -0.67% -6.56%
open 40% SingleBelt 0.00% -7.19% 4.45%
closed 40% SingleBelt 1.74% -2.48% 4.61%
5 Sedan 2 open 100% 5 Belt 0.00% -1.87% -0.37%
blanked 100% Fixed 1.57% -26.38% 9.84%
6 Sedan 3 closed 100% Fixed 2.35%
open 40% SingleBelt 0.32% -2.27% -2.27%
closed 40% SingleBelt 2.03% -1.35% 2.03%
7 Estate1 open 40% SingleBelt -0.32% 11.04% 26.62%
8 Estate2 open 100% 5 Belt -0.95% -3.81% -3.17%
9 Hatchback1 open 40% SingleBelt 3.09% 7.21% 19.75%
10 Hatchback2 open 100% 5 Belt 2.18% -22.55% 12.00%
11 SUV 1 open 40% SingleBelt 0.81% 6.59% -16.76%
12 NASCAR 1 40% SingleBelt 2.22%
13 NASCAR 2 open 40% SingleBelt -1.25% -32.67% -10.47%
14 Sem i-Truck1 open 12.5% SingleBelt 0.19%
15 LightTruck1 open 20%% SingleBelt -0.38% -5.09% -10.38%
1.2% 9.37% 9.24%AverageErrorM agnitude
Scale
Ground
Sim ulation
CoefficientsVehicleNo. VehicleM odel
Grille
(open,
closed,
blanked)
W ind TunnelData Elem ents
CD CLF CLR
21 Sem i-Truck2 open 0.000 0.125 SingleBelt 0.19%
open 0.000 0.125 SingleBelt -1.13%
open 6.000 0.125 SingleBelt 2.63%
open 6.000 0.125 SingleBelt 3.45%
open 6.000 0.125 SingleBelt 3.45%
open 0.000 0.125 SingleBelt 2.25%
open -6.000 0.125 SingleBelt 4.85%
open 9.000 0.125 SingleBelt 2.50%
open -9.000 0.125 SingleBelt 3.13%
open 9.000 0.125 SingleBelt 0.00%
open 9.000 0.125 SingleBelt 2.06%
22 LightTruck2 open 0.000 0.125 SingleBelt -0.38% -5.09% -10.38%
open 6.000 0.125 SingleBelt 2.69% -0.36% -17.95%
open 3.000 0.125 SingleBelt 1.47% -3.87% 14.73%
23 Sem i-Truck3 open 0.000 0.125 SingleBelt 0.57%
open 3.000 0.125 SingleBelt 4.13%
open 6.000 0.125 SingleBelt 4.98%
open 9.000 0.125 SingleBelt 1.11%
24 Sem i-Truck4 open 0.000 0.125 SingleBelt 5.86%
2.5% 3.11% 14.35%
Yaw
AverageErrorM agnitude
Scale
Ground
Sim ulation
CoefficientsVehicleNo. VehicleM odel
Grille
(open,
closed,
blanked)
W ind TunnelData Elem ents
• Target is a best practice that
delivers drag coefficient errors
less than 2% for passenger cars,
and 4% for heavy trucks.
21. Conclusions
• The result of this project is a set of best practices that
consistently delivers drag coefficient error magnitudes
less than 2% for passenger cars, and 4% for heavy
trucks.
• The CFD results have been heavily validated in a range
of wind tunnels, and for a variety of different vehicle
shapes.
• For typical mesh sizes of 50-80 million cells, running on
144 cores, turnarounds of 16-24 hours are the median.
This is considered to be extremely competitive when
compared to other commercial CFD codes.
Editor's Notes
Notes:
I decided to add this slide here, because the customer list is very important to show to the people which do not know us.