Edward Tinoco

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    Copyright 2009 Boeing. All rights reserved.

    The Impact of High PerformanceComputing and Computational

    Fluid Dynamics on Aircraft

    Development

    Edward N TinocoTechnical Fellow

    Ena!ling Technology " #esearch

    Airplane Configuration$ Integration " Performance

    %oeing Commercial Airplanes

    Copyright 2009 Boeing. All rights reserved.

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    Copyright 2009 Boeing. All rights reserved.

    Computational Fluid Dynamics &CFD'

    Tools for Aerodynamic Development

    of Aircraft Configurations

    Flight Test (ind Tunnel

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    Copyright 2009 Boeing. All rights reserved.

    Direct Numerical )imulation

    *arge Eddy )imulation

    Detached Eddy )imulation w+#AN)

    #eynolds Averaged Navier,)to-es

    Aerodynamic flows are characteri.ed as compressi!le$

    viscous &high #eynolds num!er tur!ulent' flows

    Computational Fluid Dynamics

    Practical

    *imit for

    CompleteAirplane

    Applications

    Increa

    sing

    Com

    putatio

    nalC

    omple/ity

    $

    Dec

    reasin

    gEm

    piricism

    Euler

    Full Potential

    (ith Coupled %oundary *ayer

    *inear Potential &Panel 0ethods' 12345s

    1264,745s

    12745s

    12245s

    84445s

    849:

    8474

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    Copyright 2009 Boeing. All rights reserved.

    127: 1224 122: 8444 844: 8414

    666 6;6N< 676

    81= thic-er faster wingthan 6:6$ 636 technology

    %est economics in class

    Highly constrained wingdesign Faster wing than

    6;6,;44 Highest sellingcommercial airplane ever

    0ultipointoptimi.ation

    design

    Faster and more effi,cient than previous

    medium si.e aircraft

    696,7

    lowest operatingcosts and !est

    economics of anylarge airplane

    1 P 144 P14 P

    ?nstructuredAdaptive

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    Copyright 2009 Boeing. All rights reserved.

    (hat is the 0easure of alue in

    Computational Fluid DynamicsB

    The value of reduced wind tunnel testing due to the use of CFDIn the past 84 years the use of CFD has provided significant cost

    savings

    (indT

    unnelHours

    (indTunnelHours

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    Copyright 2009 Boeing. All rights reserved.

    (hat is the 0easure of alue in

    Computational Fluid DynamicsB

    The value of reduced wind tunnel testing due to the use of CFDIn the past 84 years the use of CFD has provided significant cost

    savings This is a small fraction of the value CFD delivered

    A much greater value of CFD in the Commercial arena isGGG

    The added value of the product due to the use of CFDAchieving design solutions that are otherwise unreacha!le

    )hortening the design development process

    T getting it right the first time results in

    ery lengthy and costly development to fi/ it

    Possi!le cancelation+termination of the program

    Putting the Company at ris-

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    Copyright 2009 Boeing. All rights reserved.

    E/tra 0aterial

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    %oeing Puget )ound

    HPC Environment

    8441

    Cray T916

    SGI rigin

    !0.100 T"lops

    #$ll %otential & B'

    ( e.g. Tranair

    8442

    Cray )1

    %C *l$sters

    !+0 T"lops

    ,avier-Stoes

    ( e.g. C#/&& C#'/

    34#'5

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    Copyright 2009 Boeing. All rights reserved.

    CFD Contri!utions to 676

    High,)peed (ing

    Design Ca! Design

    Engine+Airframe

    Integration

    Inlet Design

    Inlet Certification

    E/haust,

    )ystem Design

    Ca!in

    Noise

    (ing,%odyFairing Design

    ertical Tail and

    Aft %ody Design

    Design For

    )ta!ility "

    Control

    High,*ift (ing

    Design

    AP? Inlet

    And Ducting

    EC) InletDesignAP? and Propulsion

    Fire )uppression

    Nacelle Design

    Thrust,#everser

    Design Community

    NoiseDesign for F>D

    Prevention

    Aeroelastics

    Icing

    Air,Data

    )ystem

    *ocation

    orte/

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    Copyright 2009 Boeing. All rights reserved.

    Cost and Flowtime Characteristics of

    (ind Tunnels and CFD

    >ne complete airplane development reuires a!out :4$444 to>ne complete airplane development reuires a!out :4$444 to

    144$444 aerodynamic simulations144$444 aerodynamic simulations

    Today Desired Future )tate

    14 144 1$444 14$444 144$444

    Cost$

    Flowtime

    Num!er of )imulations

    14 144 1$444 14$444 144$444

    Num!er of )imulations

    CFD Design$ 0ost

    Data %ase %uilding

    (ind Tunnel

    alidation)pecial

    Conditions

    CFD

    (indTunnel

    Data %ase%uilding

    The use of new CFD is driven !y desperationDesperation to remain competitiveJ

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    Closing Thoughts

    CFD e/ists to ena!le new solutions to pro!lems$ reduce airplanedevelopment cost$ and reduce time to mar-et

    CFD can allow you to safely e/plore areas of the flight regime

    without putting a pilot at ris-

    CFD can allow you to analy.e conditions for which physical

    simulation is either very e/pensive or not possi!le$ such ashypersonic propulsion systems and full flight #eynolds num!er

    testing

    Accuracy$ ro!ustness and timeliness are the -eys to acceptance

    and use in an industrial environment

    Impediments applications that do not scale well &to 14445s of

    processors with sufficient memory' this is scienceK resources to

    run 1444s of flight conditions on 1445s of processors this is the

    !usiness of engineering

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