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1 DIPARTIMENTO DI INGEGNERIA AEROSPAZIALE KTH Stockholm, 19/3/2004 The Influence of Aerodynamics on the Design of High-Performance Road Vehicles - Part 2 Guido Buresti Department of Aerospace Engineering University of Pisa (Italy)

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

The Influence of Aerodynamics on the Design ofHigh-Performance Road Vehicles - Part 2

Guido BurestiDepartment of Aerospace Engineering

University of Pisa (Italy)

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

CONTENTS

ELEMENTS OF AERODYNAMICS

AERODYNAMICS OF CARS

AERODYNAMICS OF HIGH-PERFORMANCE CARS

DESIGN TOOLS

CONCLUSIONS AND FUTURE DEVELOPMENTS

AERODYNAMICS AT FERRARI AUTO

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Experimental techniques

Design Tools

Specific wind tunnels for automotive research

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

The Ferrari Gestione Sportiva wind tunnel

Experimental Techniques

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Experimental Techniques

The Ferrari Gestione Sportiva wind tunnel

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Experimental Techniques

The Ferrari Gestione Sportiva “small” wind tunnel

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Design Tools

Numerical solution of the equations of fluid dynamics(Navier-Stokes equations)

Basic method : Direct Numerical Simulation (DNS)

For typical application conditions DNS is not possible!

Reynolds-averaged Navier-Stokes equations (RANS)

Numerical techniques

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Numerical Techniques

Reynolds-averaged Navier-Stokes equations (RANS)

“Commercial” codes are used (FLUENT, STAR-CD)

Good qualitative results, and even quantitative, if codes arevalidated with experimental data for the analysed class of bodies

Computing times: from a few hours to several days according to complexity of configuration and available computational resources

A good aerodynamic competence is necessary

Good for comparisons between different configurations

Good indications on physical phenomena

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Examples of RANS numerical results

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Examples of RANS numerical results

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Examples of RANS numerical results

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Examples of RANS numerical results

-4

-3.5

-3

-2.5

-2

-1.5

0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4

CL

h/c

Analysis of download of a front F1 airfoil withvarying distance from the ground

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Examples of RANS numerical results

Discretization of vehicle and

computational grid

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Examples of RANS numerical results

Velocity magnitude

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Examples of RANS numerical results

Pressures

Streamlines

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Examples of RANS numerical results

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Examples of RANS numerical results

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Aerodynamics at Ferrari Auto

0.32

0.34

0.36

0.38

0.4

0.42

0.44

-0.3

-0.2

-0.1

0

0.1

0.2

0.3Data 7

308 328 348 355 360

C z

Cx

1976 1984 1989 1994 1999

Aerodynamic evolution of Ferrari production cars

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Aerodynamics at Ferrari Auto

142

-179

-37

144

184

308 328 348 355 360

UploadDownload

kg

Lift Kg @ 300Km/h

Aerodynamic evolution of Ferrari cars

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Aerodynamics at Ferrari Auto

Underbody and aerodynamic coefficients of F360 Modena

Ant: - 0.11

Post: - 0.13

CZ = - 0.240CZ = - 0.240

CX = 0.335CX = 0.335

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Cooperation between DIA and Ferrari Auto

Since 1989

Graduation theses on research topics of interest for Ferrari

Solution of specific design problemsInvolvement of DIA in the development and utilization ofnew design tools

Since 2000 - General agreement DIA - Ferrari:

Working tools:

Research contracts on specific problems

DIA is reference for research and innovation in aerodynamics

DIA directly cooperates in the design of new cars

Characterization of new wind tunnel

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Cooperation between DIA and Ferrari Auto

DIA cooperated in the aerodynamic design of:

550 360

Enzo 612 …

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Cooperation between DIA and Ferrari Auto

Some topics:

Particular measurement methodsDirect measurement of vorticitySurface visualization

Basic investigations of common interestWall effects in wind tunnels

Effects of afterbody rounding

Aerodynamics of wheelhouses

Common research projectDevelopment of a numerical procedure for the optimizedpreliminary aerodynamic design of new cars

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Aerodynamics of wheelhouses

Type of Flow

Strong couplingwith underbody

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Aerodynamics of wheelhouses

Nomenclature

CeilingCeiling front fillet

Ceiling rear fillet

Front ramp

Rear ramp

Back wall

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Aerodynamics of wheelhouses

Different types of wheelhouse were analysed fordifferent car attitudes relative to the ground

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Aerodynamics of wheelhouses

Wind tunnel test campaign

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Aerodynamics of wheelhouses

RESULTS

Modifications to the geometry of wheelhouses were devisedwhich provided significant improvements

A strong correlation exists between wheelhouse geometryand underbody aerodynamics

An improvement of the wheelhouses implies a carefulanalysis of the flow on the car underbody,

specially of the outflow from the front wheelhouse

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

Objective of an aerodynamic optimization procedure:

MINIMIZING AN OBJECTIVE FUNCTIONlinked to the car aerodynamic performance

• Geometrical (style)

• Aerodynamic

• Technological

TAKING A SERIES OF “CONSTRAINTS” INTO ACCOUNT:

To devise a NEW GEOMETRY OF THE CAR

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

GeometricDescription

MeshLoads

OptimizationLoop

Gridgenerator

Solver code

Optimization code

Final Geometryand Loads

Output

Scheme of an optimization procedure

Optimized aerodynamic design

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

The evaluation of the aerodynamic loadsmust be repeated many times

The aerodynamic solver must be “unexpensive”as regards computational time, but sufficiently accurate

It is impossible (for the moment) to use codes for the solutionof the Navier-Stokes equations (even RANS)

Modified “potential” methods

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

“Potential” methods

Are much less expensive than RANS methods, but inprinciple may be applied only to “aerodynamic” bodies

Investigations carried out by DIA showed thatthey may be used also for car shapes

if the flow is attached until the body rear base and if theeffect of the separated wake is adequately taken into account

However…

The wake is modelled as a suitable continuation of the body(wake model)

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

The car surfaceis divided in two parts

forebody base

A “fictitious afterbody”is evaluated, using the“wake model”

The “computational body” is:the forebody +

the “fictitious afterbody”

Computational body

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

A WIND TUNNEL EXPERIMENTAL CAMPAIGNWAS CARRIED OUT TO VALIDATE THE PROPOSED

SIMPLIFIED LOAD EVALUATION PROCEDURE

The shape and dimensions of the model were such that itcould be considered a normal production car in 1:2.5 scale

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Validation of the computational code

• The comparison is very good• The agreement extends to the end of the body, showing that

the wake model works adequately

-1

-0.5

0

0.5

1

-500 0 500 1000

HIPEROAD y

0

200

400

600

800

1000

x (mm)

cp

-1

-0.5

0

0.5

1

-500 0 500 1000

Experimental y

0

200

400

600

800

1000

x (mm)

cp

Optimized aerodynamic design

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

Validation of the optimization procedure

VERTICAL LOADOBJECTIVE FUNCTION :

• Maximum aerodynamic drag• Maximum displacement

(3 cm in real scale)

CONSTRAINTS:

THE WHOLE OPTIMIZATION PROCEDUREREQUIRED A ONE DAY WORK

The “potential” code with wake model was used

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

OriginalModel

OptimizedModel

Comparison between original and optimized models

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

Validation resultsWind tunnel experimental data

Basic Geometry Optimized GeometryCz

Cx

0.1760.185

0.1410.181

Load variations @ 280 Km/h

Fz = - 28 kg Fx = - 3.5 kg

3 HP16 cm x 1.5 mWing

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Optimized aerodynamic design

The aerodynamic optimization procedure has been introduced inthe standard design process of the new Ferrari production cars

Style proposal (Pininfarina)

Analysis with optimization procedure (Ferrari)

Modification proposals

New style proposal

Model construction and wind tunnel tests

Approval

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Conclusions

The synthesis of all the Ferrari aerodynamic know-how …

Ferrari Enzo

Cz ≅≅≅≅ -1.0

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Conclusions

The cooperation between DIA and Ferrari has produced:

• Increase in the Ferrari internal know-how and consequentdirect involvement of Ferrari in the styling process of thenew production cars

The expected future:• Increased direct involvement of DIA in the design process of

new production cars

• Introduction at DIA of new basic aerodynamic researchactivities with applications in the automotive industry

• Opening of new occupational perspectives for graduated students

• New interesting research topics

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Conclusions

A good aerodynamic design requires:

• High basic and specific aerodynamic competence

• Search for physical comprehension

Clear and “realistic” definition of the aerodynamic specificationsand of the technological and style constraints

Strong interaction between aerodynamic, style and productiondepartments since the initial stages of the design process

• Integrated design (team work):

• Capitalization of acquired know-how

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

Future developments

Some future research topics:

• Increased know-how on the use of CFD (Navier-Stokessolvers) and their introduction in the optimization process

• Aerodynamics of cooling systems

• Study of “non-conventional configurations”

- locally-separated flows and vortical structures

• Increased understanding of and development of methods forthe useful management of:

- base flows (base drag)

- interference effects

to produceknow-howto be usedwhen neededfor new styles

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DIPARTIMENTODI INGEGNERIAAEROSPAZIALE

KTH Stockholm, 19/3/2004

THANK YOU FORYOUR ATTENTION!