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Aerodynamics of Cars

Jun 01, 2018

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    Aerodynamics of carsDrag reduction

    Alessandro Talamelli

    Johan Westin

    Mekanik/KTH

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    Outline

    General remarks on drag of cars

    • How to analyse dragLocal origins of drag

    • Individual details and their contribution to dragEx. Optimisation of Opel Calibra

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    Flow around a car

    • Car=relatively bluff body(cD=0.25-0.45)

    • Two types of separation1) Quasi 2D wakes2) Longitudinal vortices

    • Rear end determines thewake structure

    1) Square back

    2) Fast back3) Notch back

    • Underbody flow and wheels• Interactions – ground effect

    4

    Drag and Lift

    • Drag and lift normally related (lift generates drag)• Wing theory: Drag = profile drag (form drag + friction

    drag) + induced drag (induced drag from wingtipvortices)

    • Cars: low aspect ratio (Λ0.4)• Interaction between tip vortices and the central flow

    c Di = k  c L

    2

    ΛΛ =

      b2

     A plan

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    Approaches to analyse drag I

    Examine the physical mechanisms

    • Identify separation regions• Measure pressure and wall-shear stress• Drag obtained from surface integral

    • Lot of experimental data needed (unrealistic)• It is possible to find the local origins of drag

     D =   psinϕ  dS +   τ  w cosϕ  dS 

    6

    •Usually possible forsimple bodies (seefigure)

    •Problem: in real carsdifferent components

    interact!

    Approaches to analyse drag II

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    Wake analysis

    • Control volume approach + momentum theorem• Energy assessment!! Stationary wall: must subtract contribution fromwall boundary layer

    • Extensive measurements needed (costly)• Need of traversing mechanism

    c D A =   (1− c ptot )dS −   1− u

        

        

    2

      dS +  v

        

        

    2

    +  w

        

        

      

     

      

      dS 

    Approaches to analyse drag III

    8

    Local origins of drag - Front end I

    •Localseparation lesspronouncedsuction peak -increased drag

    •Small edgeradius enoughto reduce localdrag

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    • Optimization of the frontof Golf I

    • Small radii can givesignificant drag reduction

    Local origins of drag - Front end II

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    • Drag reduction due to hoodangle (α)saturatesBUT: Combination effect of

    hood angle & front radius!

    • Increased angle of windshield (

    δ) can reduce drag

    • δ60° => visibility andtemperature problems

    • indirect influence on drag: – Influence flow around A-pillar

     – Smaller suction peak at the junction to the roof

    Local origins of drag - Angle of hood andwind shield I

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    • 3D-separation (vortex)• Wind noise• Water and dirt

    deposition

    Local origins of drag - A-pillar

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    • Mainly friction drag (flow isgenerally attached)

    • Increased camber givelarger radii =>reduced

    suction peaks

    • Negative angle of roof =>reduced wake

    • Problems: large front areaand/or smaller internalspace

    Local origins of drag – Roof and Sides

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    Local origins of dragUnderbody flows

    • Complex flow• Flow angles important• Avoid obstacles (stagnation)• Return of cooling air can

    influence

    • Large improvement by rearpanels

    • Also effect on lift

    Ahmed (1999)

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    Local origins of drag - Rear End

    Boat tailing

    Mair: axisymmetric body

    Mercedes 190Angle ca 10°

    •Increase base pressure•Reduce base area•Minor improvements byfurther extension of thebody (x/d > 5)

    •Squareback vehicles:lower the roof

    •Flow devices (Air intakes,wings)

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    Boat-tailed underbody

    Local origins of drag - Rear End II

    •Requires smoothunderbody

    •Decreased drag formoderate diffuser angles

    •Reduction in lift

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    Fastback/squareback

    • Basic experiments =>understanding of rear end flow• Drag due to strong side vortices• Vortex break-up above critical slant angle

    Morel (1976) Bearman (1979)

    Local origins of drag - Rear End III

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    • Prismatic body near ground (qualitatively similar results)• Critical slant angle ca 30°• Drag minimum at ϕ15º (coupé)

    Bearman (1982)

    Morel (1976)

    Fastback/squareback

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    • Bi-stable separation aroundcritical angle (ϕ30º)

    • ϕ>30º: reduced drag andflow conditions similar to asquare back

    • ϕ>30º: Vortices are weakerand with opposite rotational

    direction than ϕ

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    Rounded rear edges

    • Previous findings based on bodies with fairlysharp edges

    • Rounded side edges => no fixed separationpoint

    • Rounded rear => optimum base height morerelevant than optimum slant angle

    • Also: the base height influence by sloping sideedges

    20

    Notchback

    • Interaction – quasi-2D separation

     – 3D vortices

    • Several geometricalparameters

    • Also influenced by – Radius roof-window

     – Shape of C-pillar

     – Rear end of trunk

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    Flow in the “dead water region”

    • Counter rotating vortices(try to identify during PIV-

    lab)

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    Sensitivity to side wind

    • Wake-analysis behind anotchback (Cogotti 1986)

    • Total-pressure distributionshow strong influence of

    small yaw angles (β=0,

    0.5°& 1°)• Bi-stable flow at β= 0.5°

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    • Attempt to explainasymmetric wake

     – A-pillar vortices interact withrear vortices

     – Very small yaw angleschange the relative strengthof A-pillar vortices

    • Symmetric flow patternunlikely on three-box config.

    Sensitivity to side wind II

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    Mechanism of a 2D-diffuser

    • Pressure increases as longas flow not separated

    • Max diffuser length longerfor small diffuser angles

    • Is the analogy with a 2Ddiffuser really correct?

    • (Can explain reduced drag,but not reduced lift)

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    Aspects of underbody diffuser

    Rear end underbody diffuser brings up thevelocity below the car (normally reduces lift)

    Higher velocity below the car changes flowangles around the wheels

    • Reduced drag due to the wheels• Requires a smooth underbody to avoid drag from

    obstacles

    Underbody diffuser reduces the base area of thevehicle (can reduce drag)

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    Underbody shaped for downforce I

    Ferrari 360 Modena

    • “Venturi-tunnel” formax downforce

    • Smooth underbody

    • No spoilers• 5400 hours in wind-tunnel (source:

    Teknikens Värld 11/99)

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    Underbody shaped for downforce I1994 1999

    F355360 Modena

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    Wheels

    • Up to 50% of the drag of astreamlined car

    • Wheels are not streamlined – 3 vortex pairs

     – Influenced by ground androtation

    • Local flow is yawed (15°) – Separation on the outer side

     – Water drops sucked out

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    Wheels (contd)

    • Force on a rotating wheelchanges sign when contact with

    ground

    • Lift force due to wheel rotationfor a free-standing wheel

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    Wheels (contd)

    • How does the flow in thewheel-housings look like?

    • Wheel-housings

     – Smaller=better – Both lift and drag reduced

     – Largest effect on lift (see e.g.Cogotti 1983)

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    Influence of wheels on Audi A3

    • 30-35% of drag due to wheels + wheel arches• Ca 25% only due to wheels From Pfadenhauer,Wickern & Zwicker (1996)

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    Spoilers

    Front spoiler

    Hucho (1998)

    +Reduced drag

    +Reduced front axle lift

    +Improved cooling air flow

    •Reduced flow rate underthe car

    •Low pressure regionbehind the spoiler

    •Optimization needed

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    Rear spoiler+ Reduced drag

    (sometimes)

    + Reduce rear axle lift

    • Higher cP in front of thespoiler

    • Increased spoiler heightincreases the lift, but

    also drag

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    Miscellaneous

    • Cooling air flow:cD0.02-0.06

    • Side mirrors: cD0.01

    • Antenna: cD0.001• Roof racks: up to 30-

    40% increase in cD

    • Ski box: Why are theyshaped in this way??

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    Potential fields for drag reduction

    More focus on underbody and wheels

    Active reduction of the dead-water region

    • Base bleedSeparation control

    • Boundary layer suction?

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    Discrepancies in cD

    Different cD depending on equipment

    • Tire width• Engine type (cooling air flow)• Ground clearance (load dependent)

    • Angle of attack (load dependent)• Additional spoilers etc.

    Official cD values “corrected”

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    Aerodynamic optimization of Opel Calibra

    • Front spoiler heightoptimization

     – Determined by minimumground clearance

    From Emmelmann et al (1990)

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    • Rear end optimization(1:5 scale model)

    • Rear end tapering• Decklid height optimization

     – Interdependent effect of

    decklif height and rear endtapering

     – Large number ofparameter tests needed

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    • cD0.28 at this time• Wake analysis (total

    pressure) and flow vis.

     – No noticeable tip vortices

     – “Ears” due to A-pillars

     – Wide wake close to ground

     – 30° flow angle at frontwheels

    • Drag reduction by – Reduced spoiler height in

    the centre

     – Increased spoiler height infront of wheels

     – Lower the door sills

    40

    • Further aerodynamical development – Anti-contamination lips

     – Cooling air inlets (cD=0.014 for air passing throughfront end)

    Before (cD0.28) After (cD0.26)