Alterations of Formula 3 Race Car Diffuser Geometry for Optimised Downforce

Similar documents
CFD Study on the Diffuser of a Formula 3 Racecar

Turbulence Modeling in CFD Simulation of Intake Manifold for a 4 Cylinder Engine

ENHANCEMENT OF AERODYNAMIC PERFORMANCE OF A FORMULA-1 RACE CAR USING ADD-ON DEVICES B. N. Devaiah 1, S. Umesh 2

The Influence of Aerodynamics on the Design of High-Performance Road Vehicles

Numerical Simulation of the External Flow Field. Around a Bluff Car*

Basics of vehicle aerodynamics

COMPUTATIONAL FLOW MODELLING OF FORMULA-SAE SIDEPODS FOR OPTIMUM RADIATOR HEAT MANAGEMENT

TWO-DIMENSIONAL FINITE ELEMENT ANALYSIS OF FORCED CONVECTION FLOW AND HEAT TRANSFER IN A LAMINAR CHANNEL FLOW

Using CFD to improve the design of a circulating water channel

CFD SIMULATION OF SDHW STORAGE TANK WITH AND WITHOUT HEATER

A. Hyll and V. Horák * Department of Mechanical Engineering, Faculty of Military Technology, University of Defence, Brno, Czech Republic

CFD Analysis of Supersonic Exhaust Diffuser System for Higher Altitude Simulation

The Influence of Aerodynamics on the Design of High-Performance Road Vehicles

Investigation of Turbulence Created by Formula One Cars with the Aid of Numerical Fluid Dynamics and Optimization of Overtaking Potential

CFD Analysis on Airfoil at High Angles of Attack

Eco Pelmet Modelling and Assessment. CFD Based Study. Report Number R1D1. 13 January 2015

Flow Physics Analysis of Three-Bucket Helical Savonius Rotor at Twist Angle Using CFD

Performance Comparison of a Vertical Axis Wind Turbine using Commercial and Open Source Computational Fluid Dynamics based Codes

Application of CFD Simulation in the Design of a Parabolic Winglet on NACA 2412

CFD analysis for road vehicles - case study

Ravi Kumar Singh*, K. B. Sahu**, Thakur Debasis Mishra***

AN ABSTRACT OF THE THESIS OF

INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING AND TECHNOLOGY (IJMET)

CFD Analysis of Swept and Leaned Transonic Compressor Rotor

The influence of mesh characteristics on OpenFOAM simulations of the DrivAer model

Practice Problems on Boundary Layers. Answer(s): D = 107 N D = 152 N. C. Wassgren, Purdue University Page 1 of 17 Last Updated: 2010 Nov 22

THE CFD SIMULATION OF THE FLOW AROUND THE AIRCRAFT USING OPENFOAM AND ANSA

CFD Based Air Flow and Contamination Modeling of Subway Stations

A Method for Generating Electricity by Fast Moving Vehicles

Flow in data racks. 1 Aim/Motivation. 3 Data rack modification. 2 Current state. EPJ Web of Conferences 67, (2014)

FAN PROTECTION AGAINST STALLING PHENOMENON

DESIGN AND FLOW VELOCITY SIMULATION OF DIFFUSER AUGMENTED WIND TURBINE USING CFD

Dimensional analysis is a method for reducing the number and complexity of experimental variables that affect a given physical phenomena.

PRESSURE DROP ANALYSIS OF INLET PIPE WITH REDUCER AND WITHOUT REDUCER USING CFD ANALYSIS

CFD ANALYSIS OF RAE 2822 SUPERCRITICAL AIRFOIL AT TRANSONIC MACH SPEEDS

AERODYNAMIC ANALYSIS OF BLADE 1.5 KW OF DUAL ROTOR HORIZONTAL AXIS WIND TURBINE

NUMERICAL ANALYSIS OF THE EFFECTS OF WIND ON BUILDING STRUCTURES

(1) 2 TEST SETUP. Table 1 Summary of models used for calculating roughness parameters Model Published z 0 / H d/h

ME6130 An introduction to CFD 1-1

Handheld Shock Control Design Guide

HEAT TRANSFER ANALYSIS IN A 3D SQUARE CHANNEL LAMINAR FLOW WITH USING BAFFLES 1 Vikram Bishnoi

EXPERIMENTAL ANALYSIS OF HEAT TRANSFER ENHANCEMENT IN A CIRCULAR TUBE WITH DIFFERENT TWIST RATIO OF TWISTED TAPE INSERTS

Swissmetro travels at high speeds through a tunnel at low pressure. It will therefore undergo friction that can be due to:

Aerodynamic Analysis. Estimation of aerodynamic performance from constant speed and coast down testing

Formula 1 Aerodynamic Assessment by Means of CFD Modelling

Navier-Stokes Equation Solved in Comsol 4.1. Copyright Bruce A. Finlayson, 2010 See also Introduction to Chemical Engineering Computing, Wiley (2006).

STUDY OF FRONT WING OF FORMULA ONE CAR USING COMPUTATIONAL FLUID DYNAMICS

F1 Fuel Tank Surging; Model Validation

2. Parallel pump system Q(pump) = 300 gpm, h p = 270 ft for each of the two pumps

Aerodynamic Department Institute of Aviation. Adam Dziubiński CFD group FLUENT

Hydrodynamic Loads on Two-Dimensional Sheets of Netting within the Range of Small Angels of Attack

CFD Analysis of a butterfly valve in a compressible fluid

2013 Code_Saturne User Group Meeting. EDF R&D Chatou, France. 9 th April 2013

Pressure in Fluids. Introduction

. Address the following issues in your solution:

M1. (a) (i) 4.5 allow 1 mark for correct substitution i.e

CFD STUDY OF TEMPERATURE AND SMOKE DISTRIBUTION IN A RAILWAY TUNNEL WITH NATURAL VENTILATION SYSTEM

Computational Modeling of Wind Turbines in OpenFOAM

SINGLE TRAIN PASSING THROUGH A TUNNEL

AN EFFECT OF GRID QUALITY ON THE RESULTS OF NUMERICAL SIMULATIONS OF THE FLUID FLOW FIELD IN AN AGITATED VESSEL

Computational Fluid Dynamics or Wind Tunnel Modeling?

Longitudinal and lateral dynamics

CFD ANALAYSIS OF FLOW THROUGH A CONICAL EXHAUST DIFFUSER

Finding Drag Coefficient using Solidworks Flow Simulation

Using Computational Fluid Dynamics (CFD) for improving cooling system efficiency for Data centers

Express Introductory Training in ANSYS Fluent Lecture 1 Introduction to the CFD Methodology

Experiment 3 Pipe Friction

XFlow CFD results for the 1st AIAA High Lift Prediction Workshop

NACA FINDING LIFT COEFFICIENT USING CFD, THEORETICAL AND JAVAFOIL

FLow pattern around cable and its aerodynamic characteristics in critical Reynolds number range

Numerical Investigation of Heat Transfer Characteristics in A Square Duct with Internal RIBS

COMPUTATIONAL FLUID DYNAMICS (CFD) ANALYSIS OF INTERMEDIATE PRESSURE STEAM TURBINE

GEOMETRIC, THERMODYNAMIC AND CFD ANALYSES OF A REAL SCROLL EXPANDER FOR MICRO ORC APPLICATIONS

Keywords: CFD, heat turbomachinery, Compound Lean Nozzle, Controlled Flow Nozzle, efficiency.

A Comparison of Analytical and Finite Element Solutions for Laminar Flow Conditions Near Gaussian Constrictions

ACCELERATION CHARACTERISTICS OF VEHICLES IN RURAL PENNSYLVANIA

CFD Application on Food Industry; Energy Saving on the Bread Oven

Dr.A.K.Shaik Dawood. N.V.Kamalesh. Department of Mechanical Engineering, Associate Professor, Karpagam University, Coimbatore , India.

Rapid Design of an optimized Radial Compressor using CFturbo and ANSYS

O.F.Wind Wind Site Assessment Simulation in complex terrain based on OpenFOAM. Darmstadt,

Head Loss in Pipe Flow ME 123: Mechanical Engineering Laboratory II: Fluids

Accurate Air Flow Measurement in Electronics Cooling

In order to describe motion you need to describe the following properties.

SIMPLIFIED METHOD FOR ESTIMATING THE FLIGHT PERFORMANCE OF A HOBBY ROCKET

Study on Drag Coefficient for the Flow Past a Cylinder

Dynamic Process Modeling. Process Dynamics and Control

MAXIMISING THE HEAT TRANSFER THROUGH FINS USING CFD AS A TOOL

CHAPTER 6 WORK AND ENERGY

C B A T 3 T 2 T What is the magnitude of the force T 1? A) 37.5 N B) 75.0 N C) 113 N D) 157 N E) 192 N

Name Partners Date. Energy Diagrams I

OPERATING FANS IN PARALLEL IN VIEW OF VARIABLE FLOW RATE OUTPUT

Action 9.2/Part II. Stijn Vranckx, Peter Vos VITO

DEVELOPMENT OF HIGH SPEED RESPONSE LAMINAR FLOW METER FOR AIR CONDITIONING

DIESEL ENGINE IN-CYLINDER CALCULATIONS WITH OPENFOAM

9. The kinetic energy of the moving object is (1) 5 J (3) 15 J (2) 10 J (4) 50 J

JET ENGINE PERFORMANCE. Charles Robert O Neill. School of Mechanical and Aerospace Engineering. Oklahoma State University. Stillwater, OK 74078

Development Methodologies for Formula One Aerodynamics

Transcription:

International Journal of Engineering Research and Technology. ISSN 0974-3154 Volume 6, Number 3 (2013), pp. 351-358 International Research Publication House http://www.irphouse.com Alterations of Formula 3 Race Car Diffuser Geometry for Optimised Downforce Soumya Kanta Das 1, Pavan Kumar 2 and Shweta Rawat 3 VIT University, Vellore PESIT Engineering College, Bangalore IGDTUW, IP University, Delhi. Abstract This paper deals with the aerodynamic behavior and performance of a Formula-3 Race car diffuser. The effects of operating parameters such as ride height, diffuser length and ramp angle on down-force along the straights are dealt. Even one-hundredth of a second matters a lot in Motor Racing. The Diffuser being an underbody aerodynamic component plays a vital role in enabling the car to carry speed on Track. Overtaking is an important aspect of Racing, as it helps in gaining track position and ultimately the race finish order. Hence, the above mentioned parameters are taken into consideration and its set-up changes are closely examined to improve overtaking maneuverability. Steady state conditions have been considered with the analysis of flow around a bluff body configuration due to the complexity of a complete Formula 3 car. Computational Analysis performed on a bluff body subjected to 3-D axial flow is completed using ANSYS Fluent package. Keywords: Formula 3, Diffuser, Overtaking, Computational Fluid Dynamics (CFD). 1. Introduction Aerodynamics plays a vital role in governing a Race Car s performance. Depending on circuit characteristics, the set-up can be altered to suit top speed along with minimum drag and maximum downforce. For a Racing driver the ideal set-up is normally to get the maximum amount of downforce at high speed corners and minimum drag in high speed straights, for least downforce generated. Motor Racing is highly regulated,

352 Pavan Kumar et al developed and competitive sport. Formula-3 is a class of open-wheel Formula Racing, whose technical regulations are governed by FIA. Underbody diffuser accounts to a major role in improving aerodynamic efficiency of a Formula-3 Car. The key role of a rear diffuser on a modern Race Car is to accelerate the flow under the car, creating an area of low pressure on the whole underfloor plan area. The constant density of the air at such low speeds creates a vacuum at the enlarged area of the diffuser which sucks more air from the underfloor and simultaneously slowing down the flow towards the rear during the exit in order to match it up with the ambient flow and filling the wake behind the car, also, the upward momentum is provided to the flow which further increases the downforce. The effect of varying ramp angles of diffusers on the downforce and drag coefficients is computed and pressure plots and velocity contours are plotted in CFD. 2. Set-Up and Meshing Tools Diffuser characteristics are analyzed by integrating a diffuser with an Ahmed Body, whose slant angle is made zero degree and carrying out an unstructured meshing for it on CFD package. The ramp angles were continuously increased with steps of 2 degrees. The mesh sensitivity is of 413379 nodes and 1806979 elements for a bluff body of 1044 mm long, 288 mm high and 389 mm wide. As per FIA Formula-3 technical regulations on rear body work & dimensions under Article 3 (i) overall width of the car is limited to 1850 mm. (ii) rear track width should not exceed 1540 mm. (iii) Maximum width of body work behind rear wheel center line is 900 mm. Keeping these in mind the diffuser length is set to be 350 mm according to the proportions of an actual F3 diffuser. The element size in the vicinity of the bluff body is set at 15 mm and the bluff body itself at 10 mm. A coarse meshing but a high smoothing transition is set for more precise results. K-Epsilon model is adopted for this experimentation as it s the best at speeds of 50m/s which is taken here. Figure 1: Ahmed body meshing. The computational domain which basically works as a virtual wind tunnel for the set-up is shown in figure 2.

Alterations of Formula 3 Race Car Diffuser Geometry for Optimised Downforce 353 Figure 2: Computational Domain. For speed equal to 50 m/s, the ramp angle for the diffuser is increased from 2 0 and the values of downforce and drag are computed for various angles till the angle of stall i.e. 20 0 is reached where maximum downforce is obtain and angles more than that, show the gradual decline of downforce. 3. Contour Plots 3.1 Velocity plots for 8 0 and 20 0 ramp angle From figure 3, it can observed that the velocity of air underneath the car prior to the entrance of diffuser section has a higher value. This is primarily due to the compromise in static pressure, as per Bernoulli s theorem. As the air flows passes through diffuser, its velocity decreases to maintain constant mass flow rate. Figure 3: Velocity plot at 80.

354 Pavan Kumar et al Figure 4: Velocity plot at 200. There is significant reduction in the area of low velocity towards the rear of the Ahmed body with the increase in the ramp angle and we observe that the up wash of flow is with greater velocity thus, increasing the downforce manifold. 3.2 Pressure plots for 8 0 and 20 0 ramp angle Figure 5: Pressure plot at 8 0 Figure 6: Pressure plot at 20 0 The above plots depict the pressure distribution over bluff body at two different ramp angles. In figure 6, the immense low pressure gained under the body indicates the gain in downforce as also shown in the velocity plots. 3.3 Static Pressure plot at 20 0 The pressure contour is represented for 20 ramp angle, as mentioned earlier the diffuser stalls at that angle. Negative pressure underneath & high pressure over the bluff body results in pressure differential which generates down force. Carefully observing the above contour, it can be noted that the pressure inside diffuser region is below atmospheric pressure & attains the same value only at the exit [3].

Alterations of Formula 3 Race Car Diffuser Geometry for Optimised Downforce 355 Figure 7: Static pressure plot at 20 0 3.4 Turbulent Kinetic Energy plots at 8 0 and 20 0 Figure 8: Turbulent kinetic energy at 8 0 Figure 9: Turbulent kinetic energy at 20 0 The above plot highlights the mean kinetic energy per unit mass associated with eddies in turbulent flow. It can be observed that turbulence is redistributed for the 2 nd case thus offering more drag than 8 0 ramp angle. 4. Results and Discussion 4.1 Graph showing Downforce Coefficient vs. ramp angle The Graph depicts that downforce coefficient increases linearly with the increase in ramp angle and slight decrease initiating from 16 0 angle and then ultimate stall occuring after 20 0 from where the downforce drops significantly.

356 Pavan Kumar et al Downforce coefficient (cdf) 3 2.5 2 1.5 1 0.5 0 0 5 10 15 20 25 ramp angle (Ө) 4.2 Graph showing Drag Coefficient vs. ramp angle The above graph highlights the increasing drag penalty along with the increase in downforce on increasing ramp angle. For the case of 6 o ramp angle where minimum co-efficient of drag occurs, the pressure change that occurs underneath the bluff body is smaller compared to 20 o case. Drag Coefficient (Cd) 0.9 0.8 0.7 0.6 0.5 0.4 0.3 0.2 0.1 0 0 5 10 15 20 25 RAMP ANGLE (Ө) 4.3 Graph showing C L /C D vs. ramp angle The graph shows that C L /C D declines in a range between 18-20 degrees. Though the stall angle is found to be 20 0 from the C DF vs. ramp angle graph, but we infer that C L /C D vs. ramp angle graph gives a much clearer idea about how to increase the efficiency of the diffuser. Thus, this implies that the ramp angle of 17 0-18 0 is ideal for maximum down force since in Formula 3 diffusers, drag is compromised for down force increase.

Alterations of Formula 3 Race Car Diffuser Geometry for Optimised Downforce 357 Cl/Cd 4.5 4 3.5 3 2.5 2 1.5 1 0.5 0 0 5 10 15 20 25 RAMP ANGLE (Ө) 5. Conclusion A 3-D bluff body was outlined which enabled us to understand the performance of diffuser. The geometry was simulated over a range of ramp angle 0-22 degrees, keeping the ride height constant at 30mm.For optimal performance of diffuser, 18 degree ramp angle would be the best set-up. So as to achieve maximum aerodynamic efficiency & down force. This research can be further extended in analyzing the flow over two bluff bodies subjected to slip-streaming. References [1] Article: 3 2013 Formula 3 Technical Regulations, Federation Internationale De L Automobile [2] Competition Car Aerodynamics by Simon McBeath [3] Kevin M.Peddie and Louis F.Gonzales -CFD study on the diffuser of a Formula 3 Race Car.

358 Pavan Kumar et al