9 results on '"race car"'
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2. CFD Analysis of the Location of a Rear Wing on an Aston Martin DB7 in Order to Optimize Aerodynamics for Motorsports.
- Author
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O'Driscoll, Thomas P. and Barron, Andrew R.
- Subjects
LOCATION analysis ,AERODYNAMICS ,COMPUTATIONAL fluid dynamics ,MOTORSPORTS ,WIND tunnels ,BACK exercises ,AERODYNAMICS of buildings ,SPEED - Abstract
The purpose of this study is to identify the initial lateral and vertical location and angle of attack of a GT4-style rear wing on the rear downforce for an Aston Martin DB7 Vantage, prior to installation. The tests were completed with a two-dimensional model, using the Computational Fluid Dynamics (CFD) software, Fluent Ansys. The tests were completed using a range of velocities: 60–80 mph. Optimization of the position of the rear wing aerodynamic device was permitted under the Motorsport UK rules for multiple race series. The results show that while the drag decreases the farther back the wing is located, the desired configuration for the rear wing with regard to downforce is when it is positioned ca. 1850 mm back from the center point of the car, with an attack angle of 5°. Unusually, this is to the front of the boot/rear deck, but it is remarkably similar to where Aston Martin set the rear wing on their Le Mans car in 1995, above where the rear windscreen met the boot hinge, which was based upon wind tunnel studies using a scale model. Our results suggest that while 2D simulations of these types cannot give absolute values for downforce due to aerodynamic device location, they can provide low costs, fast simulation time, and a route for a wide range of cars, making the approach accessible to club motorsports, unlike complex 3D simulation and wind tunnel experimentation. [ABSTRACT FROM AUTHOR]
- Published
- 2022
- Full Text
- View/download PDF
3. Performance of NACA Cambered and Symmetrical Airfoils as Rear Spoilers on Race Car Aerodynamic Drag & Lift: Computational Fluid Dynamics Study
- Author
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Shamudra Dey and Ranabir Saha
- Subjects
Airfoil ,Lift ,business.industry ,General Medicine ,Aerodynamics ,Computational fluid dynamics ,Drag ,Lift (force) ,Race car ,NACA ,Spoiler ,Aerodynamic drag ,business ,Geology ,Marine engineering - Abstract
In the current study, the aerodynamic effects of NACA 2412 cambered & NACA 0012 symmetric airfoils as rear spoilers on a race car were analyzed using the Computational Fluid Dynamics (CFD) technique. Overall nine simulations have been conducted: one with the flow around the simplistic high-speed sports car model with no spoiler and eight for the representation of the flow across the sports car model with spoilers constructed of NACA 2412 and NACA 0012 airfoil having -6°, -3°, +3° and +6° angles of attack, accordingly. The study was conducted using the k-epsilon method as well as for a velocity of 40 m/s. Grid independence study had been conducted and the CFD analysis had been checked by contrasting the results with the famous vehicle aerodynamics experimental study of Ahmed. Among the spoilers studied, this was found that the NACA 0012 with a +6 ° angle of attack ensures a drag reduction of 2.16% and a significant lift reduction of 111.22%. The results of the rear spoiler were described from an aerodynamics viewpoint.
- Published
- 2020
- Full Text
- View/download PDF
4. Engineering the race car wing: application of the vortex panel numerical method.
- Author
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Marqués-Bruna, Pascual
- Subjects
- *
AERODYNAMICS , *BOUNDARY layer (Aerodynamics) , *AEROFOILS , *REYNOLDS number , *AUTOMOBILE racing , *MATHEMATICAL models , *COMPUTER software - Abstract
This study examined aerodynamic properties and boundary layer stability in five cambered airfoils operating at the low Reynolds numbers encountered in motor racing. Numerical modelling was carried out in the flow regime characterised by Reynolds numbers 0.82-1.29 × 10. The design Reynolds number of 3 × 10 was used as a reference. Aerodynamics variables were computed using AeroFoil 2.2 software, which uses the vortex panel method and integral boundary layer equations. Validation of AeroFoil 2.2 software showed very good agreement between calculated aerodynamic coefficients and wind tunnel experimental data. Drag polars, lift/drag ratio, pitching moment coefficient, chordwise distributions (surface velocity ratio, pressure coefficient and boundary layer thickness), stagnation point, and boundary layer transition and separation were obtained at angles of attack from −4° to 12°. The NASA NLF(1)-0414F airfoil offers versatility for motor racing with a wide low-drag bucket, low minimum profile drag, high lift/drag ratio, laminar flow up to 0.7 chord, rapid concave pressure recovery, high resultant pressure coefficient and stall resistance at low Reynolds numbers. The findings have implications for the design of race car wings. [ABSTRACT FROM AUTHOR]
- Published
- 2011
- Full Text
- View/download PDF
5. Passive variable rear-wing aerodynamics of an open-wheel racing car
- Author
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Kajiwara, Shinji
- Published
- 2017
- Full Text
- View/download PDF
6. The Effect of Spoiler Shape and Setting Angle on Racing Cars Aerodynamic Performance
- Author
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Hesam Eftekhari, Abdulkareem Sh. Mahdi Al-Obaidi, and Shahrooz Eftekhari
- Subjects
General Computer Science ,Spoiler ,Space and Planetary Science ,Computer science ,business.industry ,General Chemical Engineering ,General Engineering ,Aerodynamics ,Structural engineering ,Aerodynamic Performance ,Race Car ,CFD ,Geotechnical Engineering and Engineering Geology ,business - Abstract
Automotive racing is one of the favorite sports of human being. There have been many developments in past decades by car engineers to improve the performance of the engine and increase the aerodynamic efficiency of the race cars to achieve a better lap time and get a better placement safely. One of the ways to improve the aerodynamic performance of a race car is to use rear spoilers. This study by using ANSYS FLUENT numerically investigated the effect of the spoiler shape and setting angle on the aerodynamic characteristics of a race car and then it was validated by conducting wind tunnel experiment. Lift and drag coefficient of NACA0012, NACA4412, and S1223 are determined in Reynold’s number of 2×105 as an airfoil and as spoiler on ERC model which is a conceptual car model inspired by Porsche 911. It was found that ERC model with spoiler would have better aerodynamic efficiency compared to ERC model without spoiler. Also, S1223 at -6 degrees was identified as the optimized configuration as it generates the highest downforce. Even though the drag coefficient at this setting angle is slightly higher, but in terms of stability and handling IT is at its best. Overall, this study would help car manufacturers, for racing and commercial purposes, to have a better insight into the effect of spoiler configuration on the aerodynamic performance of cars. Hence, the stability, handling, and efficiency of the cars can be further improved by selecting the suitable spoiler configuration.
- Published
- 2020
- Full Text
- View/download PDF
7. The influence of slipstreaming on sports prototype race car performance.
- Author
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Dominy, R G, Ryan, A, and Sime-Williams, D B
- Subjects
AERODYNAMICS ,VEHICLES ,RACING automobiles ,SIMULATION methods & models - Abstract
The effect of slipstreaming on a Le Mans ‘LM’ GTP sports racing car has been investigated using a computational lap time simulation based on new wind tunnel data. The effects of changes of the aerodynamic characteristics when slipstreaming are clearly identified and the effects of those changes have been quantified in terms of the relative performances of two cars racing in close proximity. [ABSTRACT FROM AUTHOR]
- Published
- 2000
- Full Text
- View/download PDF
8. Benchmark tests for a Formula SAE Student car prototyping
- Author
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Florin Mariasiu
- Subjects
Engine power ,Engineering ,Drag coefficient ,piezoresistive sensors ,Environmental Engineering ,business.industry ,Mechanical Engineering ,cfd simulation ,Aerospace Engineering ,Aerodynamics ,Computational fluid dynamics ,race car ,Engineering (General). Civil engineering (General) ,aerodynamic ,Formula SAE ,benchmark ,Software ,Benchmark (computing) ,General Materials Science ,TA1-2040 ,Electrical and Electronic Engineering ,business ,Simulation ,Civil and Structural Engineering ,Wind tunnel - Abstract
Aerodynamic characteristics of a vehicle are important elements in its design and construction. A low drag coefficient brings significant fuel savings and increased engine power efficiency. In designing and developing vehicles trough computer simulation process to determine the vehicles aerodynamic characteristics are using dedicated CFD (Computer Fluid Dynamics) software packages. However, the results obtained by this faster and cheaper method, are validated by experiments in wind tunnels tests, which are expensive and were complex testing equipment are used in relatively high costs. Therefore, the emergence and development of new low-cost testing methods to validate CFD simulation results would bring great economic benefits for auto vehicles prototyping process. This paper presents the initial development process of a Formula SAE Student race-car prototype using CFD simulation and also present a measurement system based on low-cost sensors through which CFD simulation results were experimentally validated. CFD software package used for simulation was Solid Works with the FloXpress add-on and experimental measurement system was built using four piezoresistive force sensors FlexiForce type.
- Published
- 2011
- Full Text
- View/download PDF
9. Investigation of the Flow Unsteadiness of Car Air-Box by Using LES
- Author
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A. Bianchi d’Espinosa, Federico Brusiani, Gian Marco Bianchi, F. Brusiani, G.M. Bianchi, and A. D’Espinosa
- Subjects
Engineering ,business.industry ,Strategy and Management ,Mechanical Engineering ,Metals and Alloys ,AIRBOX ,Aerodynamics ,Industrial and Manufacturing Engineering ,Vehicle dynamics ,Flow (mathematics) ,LES ,Fluid dynamics ,RACE CAR ,Aerospace engineering ,VOLUMETRIC EFFICIENCY INCREASE ,business ,CFD ,Large eddy simulation - Abstract
Today, high performance race car efficiency is based on a very fine equilibrium between aerodynamic efficiency, engine performance, and chassis behaviour. In particular, from the engine point of view, one way to increase the performance is to increase its volumetric efficiency. The aim of this paper is to present the application of the Large Eddy Simulation (LES) approach for the fluid dynamic analysis of a high performance race car airbox geometry. For a naturally aspired engine, the fluid dynamic optimisation of the airbox geometry means to optimise the energy conversion (from dynamic to static pressure) inside the airbox itself, therefore to increase the flow energy on the engine trumpet sections. The LES approach seems to be the best candidate to investigate such a flow since flow unsteadiness are expected to affect airbox efficiency in terms of pressure recovery. The airbox simulations were performed by using the commercial CFD code Fluent v6.3. The Wall Adaptive Local Eddy-Viscosity (WALE) Sub-Grid Scale (SGS) model was adopted together with a bounded second order central differencing scheme. The LES methodology here adopted was validated by previous works. In order to guarantee realistic fluid dynamic conditions on the airbox inlet section, a part of the car body was considered in the computational domain. Results obtained by LES simulations were analysed in terms of mean and rms evolutions of both pressure and velocity components. This study shows that, today, the LES technique is a very promising and proficient way to obtain detailed information about flow unsteadiness also on industrial cases.
- Published
- 2010
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