A Versatile Sharp Interface Immersed Boundary Method with ... · – Resolution of vortex dynamics...
Transcript of A Versatile Sharp Interface Immersed Boundary Method with ... · – Resolution of vortex dynamics...
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A Versatile Sharp Interface Immersed A Versatile Sharp Interface Immersed Boundary Method with Application to Boundary Method with Application to
Complex Biological Flows Complex Biological Flows
RajatRajat MittalMittalMechanical Engineering
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Biological FlowsBiological FlowsBiomimeticsBiomimetics and and BioinspiredBioinspired EngineeringEngineering–– What can we learn from Nature ?What can we learn from Nature ?–– How can we adapt NatureHow can we adapt Nature’’s s
solutions into engineered solutions into engineered devices/machines ?devices/machines ?
Biomedical EngineeringBiomedical Engineering–– Cardiovascular flowsCardiovascular flows–– Respiratory flowsRespiratory flows–– PhonatoryPhonatory/Speech Mechanisms/Speech Mechanisms–– Biomedical DevicesBiomedical Devices
Flapping flight
Flexible Propulsors
Drafting
Autorotation
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Inspiration from DragonfliesInspiration from DragonfliesDragonfliesDragonflies–– Existed for 350 million yearsExisted for 350 million years–– Wingspan from 2 Wingspan from 2 –– 80 cm80 cm
–– Fast and agileFast and agile
Wing DesignWing Design–– Thin, lightweight Thin, lightweight –– Vein reinforced Vein reinforced –– Pleated along chordPleated along chord–– PterostigmaPterostigma–– MicrostructureMicrostructure
Wing ConfigurationWing Configuration–– WingWing--wing interaction?wing interaction?
Wing Flexion?Wing Flexion?
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Computational ModelingComputational ModelingNeed to tackleNeed to tackle–– Complex 3D geometriesComplex 3D geometries–– Moving boundaries Moving boundaries –– Fluid Structure InteractionFluid Structure Interaction–– Resolution of vortex dynamicsResolution of vortex dynamics–– Relatively low Reynolds numbersRelatively low Reynolds numbers
Very challenging for conventional body Very challenging for conventional body fitted methods.fitted methods.
Immersed Boundary Methods Immersed Boundary Methods –– handle these problems in all their complexity.handle these problems in all their complexity.
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ViCar3DViCar3DViViscous scous CarCartesian Grid Solver for tesian Grid Solver for 3D3D Immersed BoundariesImmersed Boundaries
Simulations on nonSimulations on non--conforming Cartesian Gridsconforming Cartesian Grids–– Stationary/moving boundariesStationary/moving boundaries–– Solids/membranesSolids/membranes
Sharp Interface IBM methodSharp Interface IBM method–– No boundary forcing (No boundary forcing (PeskinPeskin et al) et al) –– 3D ghost3D ghost--cell methodologycell methodology
22ndnd Order Fractional Step SchemeOrder Fractional Step Scheme
22ndnd Order nonOrder non--dissipative central dissipative central difference schemedifference scheme–– IBM treatment also 2IBM treatment also 2ndnd order accurateorder accurate
NonNon--uniform meshesuniform meshesGeometric Geometric MultigridMultigrid for Pressure Poissonfor Pressure PoissonGlobal Global CoeffCoeff Dynamic SGS Model Dynamic SGS Model ((VremanVreman))
Journal of Computational PhysicsVolume 227, Issue 10, 1 May 2008, Pages 4825-4852
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ViCar3DViCar3DParallelizedParallelized
Extensively validatedExtensively validated
T=1T=1
T=3T=3
T=5T=5Komoutsakos & Leonard VICAR3DVICAR3D
ImpulsivelyStarted CylinderRe=1000
Mittal et al 2008, JCP
2 M pts
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Closing the Loop for Closing the Loop for CFD in Biology/Biomedical EngineeringCFD in Biology/Biomedical Engineering
Imaging Imaging (MRI, CT, Laser Scan)(MRI, CT, Laser Scan)
Geometric ModelsGeometric Models
AnimationAnimationOf Geometric ModelsOf Geometric Models
CFD/FSI SolverCFD/FSI SolverFor Complex, Moving For Complex, Moving
Organic ShapesOrganic Shapes
MimicsMimics Alias MAYAAlias MAYA
VICAR3DVICAR3D
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ViCar3DViCar3D--CapabilitiesCapabilities
• "Wake Topology and Hydrodynamic Performance of Low-Aspect-Ratio Flapping airfoil", J. Fluid Mechanics(2006) Vol 566 pp 309-343 .
•Low-dimensional models and performance scaling of a highly deformable fish pectoral fin; J. Fluid Mech. (2009), vol. 631, pp. 311–342.
•"Computational modelling and analysis of the hydrodynamics of a highly deformable fish pectoral fin." (2010) , Journal of Fluid Mechanics , doi:10.1017/S0022112009992941.
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ViCar3DViCar3D--CapabilitiesCapabilities
CFD of the dolphin kick
• "Propulsive Efficiency of the Underwater Dolphin Kick in Humans", Journal of Biomechanical Engineering, Vol. 131, May 2009
•"A computational method for analysis of underwater dolphin kick hydrodynamics in human swimming", Sports Biomechanics, 8(1), pp. 60-77, March 2009.
• "A comparison of the kinematics of the dolphin kick in humans and cetaceans", Human Movement Science, Vol.28, pp.99-112, 2009
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High Re??High Re??
• Rec = 105
• 512x256x32
• 128 CPUs
• Nonlinear dynamics and synthetic-jet-based control of a canonical separated flow. J. Fluid Mech., doi:10.1017/S002211201000042X
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Flight Maneuvers in Insects Flight Maneuvers in Insects
Side View Top ViewGravity
Maneuver: change in heading and/or speedManeuver: change in heading and/or speedInsects display a large array of maneuversInsects display a large array of maneuvers
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Flapping Frequency and ManeuveringFlapping Frequency and Maneuvering
~ /turn
T I CI C
θθ
θθ
θ θτ= +
High frequency flappers (f > 150 Hz)High frequency flappers (f > 150 Hz)–– Bees, Flies, wasps etcBees, Flies, wasps etc–– ττturn turn > 10> 10ττflap flap
–– Minute changes in kinematics Minute changes in kinematics required to execute turn. required to execute turn. (Dickinson et al)(Dickinson et al)
–– Stroke plane/amplitude/pitch angleStroke plane/amplitude/pitch angle
Low frequency flappers (f < 50 Hz)Low frequency flappers (f < 50 Hz)–– Moths, butterflies, locusts etc. Moths, butterflies, locusts etc. –– ττturn turn ~ ~ ττflapflap
–– Turns can be executed in O(1) flap if wings can produce Turns can be executed in O(1) flap if wings can produce sufficient turning moments.sufficient turning moments.
–– Does this happen??Does this happen??
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• Turning in a Monarch Butterfly• Sequence shows 1.5 flaps• >90o change in heading !• Turning distance < body size• Turn on a dime!
+
+
+
+
+
++
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How does the Butterfly do this ? How does the Butterfly do this ? Deformable WingsDeformable Wings
Wings deform significantlyWings deform significantly
Greater repertoire of wing Greater repertoire of wing kinematics.kinematics.
–– Large leftLarge left--right wing right wing asymmetriesasymmetries
What causes deformationWhat causes deformation
–– Flow and inertia induced Flow and inertia induced deformation. (deformation. (Daniels et alDaniels et al))
–– Also active deformation through Also active deformation through action of direct muscles on action of direct muscles on axillaryaxillary scleritessclerites (wing joint).(wing joint).
Perhaps even active control of Perhaps even active control of deformability ??deformability ??
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Wing Flexion:Wing Flexion:Enabler of other Flight ModesEnabler of other Flight Modes
COBRE Insect Videogrammetry Lab Moth in Climbing Flight
Clap & peel enabled bywing flexion
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Integrated ApproachIntegrated ApproachHigh Speed High Speed VideogrammetryVideogrammetry–– JHU Laboratory for JHU Laboratory for BioinspiredBioinspired EngineeringEngineering–– Tyson Hedrick Lab (UNC)Tyson Hedrick Lab (UNC)
Structural parameterization Structural parameterization ((VallanceVallance Lab, GWU)Lab, GWU)–– WingWing–– BodyBody
High Fidelity Computational Modeling of High Fidelity Computational Modeling of Aerodynamics and AeroAerodynamics and Aero--Structural InteractionStructural Interaction–– Sharp Interface Immersed Boundary MethodSharp Interface Immersed Boundary Method–– Direct and LargeDirect and Large--Eddy Simulation Eddy Simulation –– Wing deformation modeling using FEM Wing deformation modeling using FEM
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HawkmothHawkmoth in Hoverin Hover
Hedrick Lab (UNC)Hedrick Lab (UNC)
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Animated Model Rendered for CFDAnimated Model Rendered for CFD
Moth body based Moth body based on highon high--res laser res laser scan.scan.
Animation created Animation created in MAYA by in MAYA by matching high matching high speed video.speed video.
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Vortex DynamicsVortex Dynamics
Strong spiral LEV on Strong spiral LEV on downstrokedownstroke..
Vortex ring shed at the Vortex ring shed at the end of end of downstrokedownstroke from from each wing.each wing.
Weak LEV on upstrokeWeak LEV on upstroke
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Lift PredictionLift PredictionWt. of insect ~ 13.6 Wt. of insect ~ 13.6 mNmN
Average lift from CFD =15.0 Average lift from CFD =15.0 mNmN. Not bad!. Not bad!
How well does the timeHow well does the time--variation of lift compare to experiment?variation of lift compare to experiment?
Experimental determination?Experimental determination?–– Track acceleration of CM of wing, body partsTrack acceleration of CM of wing, body parts
–– Use simple dynamical model of insect to back out lift on wing.Use simple dynamical model of insect to back out lift on wing.
Fairly good prediction of peak thrust during Fairly good prediction of peak thrust during downstrokedownstroke..
Some mismatch during upstrokeSome mismatch during upstroke–– Larger cycleLarger cycle--toto--cycle variations in upstrokecycle variations in upstroke
Interestingly, upstroke is found to be quite ineffective!Interestingly, upstroke is found to be quite ineffective!
down up
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Comparison with Past Models Comparison with Past Models Liu et al (Chiba University)Liu et al (Chiba University)HawkmothHawkmoth in hoverin hoverRigid wingsRigid wingsKinematics based Kinematics based on Ellingtonon Ellington’’s data.s data.Average lift is comparableAverage lift is comparable
However simulations show However simulations show significant lift generation significant lift generation during up (back) stroke.during up (back) stroke.
Possibilities?Possibilities?–– Discrepancy in kinematicsDiscrepancy in kinematics–– Rigid versus deformable?Rigid versus deformable?
Current
Liu et al.
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Vortex Ring Impingement ExperimentsVortex Ring Impingement Experiments
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Vortex Ring Impingement: CFDVortex Ring Impingement: CFD
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Biophysics of Phonation Biophysics of Phonation
NIH R01 grant focused NIH R01 grant focused on flowon flow--structural structural interaction in larynxinteraction in larynxUnderstand the FSI Understand the FSI mechanismsmechanismsApply knowledge to Apply knowledge to enhance laryngeal enhance laryngeal surgical procedures.surgical procedures.
GeneratorGenerator(Lungs(Lungs))
VibratorVibrator((LarynxLarynx))
ResonatorResonator((Pharynx,Pharynx,
Nasal cavity,Nasal cavity,Sinuses)Sinuses)
ArticulatorArticulator((Cheek, Cheek, tongue, tongue, Teeth,Teeth,lips)lips)
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Modeling of FluidModeling of Fluid--Tissue Tissue InteractionInteraction
ViCar3D coupled to another solver that ViCar3D coupled to another solver that computes deformation of elastic structurescomputes deformation of elastic structures
Two approaches used for elastic structuresTwo approaches used for elastic structures–– FiniteFinite--Element approach Element approach –– Cartesian grid based approach (LECar3D) Cartesian grid based approach (LECar3D)
ViCar3D(Glottal Aerodynamics)
LECar3D(VF Deformation)
Aerodynamic Forces on VF
VF Displacement & Velocity
• "An immersed-boundary method for flow-structure interaction in biological systems with application to phonation", Journal of Computational Physics, 2008
•
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Structural Dynamics of VFStructural Dynamics of VF
Governing equationsGoverning equations
Model assumed in current study
Schematic showing VF substructure
cover
ligament
body
•The tissue materials are assumed to be transversely isotropic.
•Material properties are obtained from experiments (e.g., Titze et al 2000).
•Multi-property, non-homogeneous structure
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FlowFlow--Induced Vibration (FEM)Induced Vibration (FEM)Simulation DetailsSimulation Details
–– 2D Simulation2D Simulation–– Geometry based notionally on CT scan Geometry based notionally on CT scan
of human larynxof human larynx–– ViCar3D for airViCar3D for air--flowflow–– FiniteFinite--Element for VFElement for VF–– VF not fully adductedVF not fully adducted
ObservationsObservations–– KelvinKelvin--Helmholtz Helmholtz
vorticesvortices–– BistableBistable JetJet–– Sustained vibrations of vocal folds.Sustained vibrations of vocal folds.
(400K points)
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3D Vocal Fold Model3D Vocal Fold Model
• Analysis of flow-structure interaction in the larynx during phonation using an immersed-boundary method; J. Acoust. Soc. Am. 126 2 , August 2009.
• Computational Study of the Effect of False Vocal Folds on Glottal Flow and Vocal Fold Vibration During Phonation," Annals of Biomedical Engineering, Vol. 37, No. 3 pp. 625-642 March 2009
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Towards PatientTowards Patient--Specific ModelsSpecific Models
Sagittal View
Axial View
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30
Direct Computation of LowDirect Computation of Low--Mach Number SoundMach Number SoundLinearizedLinearized Perturbed Compressible Equations (LPCE)Perturbed Compressible Equations (LPCE)
0( , ) '( , )
( , ) ( , ) '( , )( , ) ( , ) '( , )
x t x t
u x t U x t u x tp x t P x t p x t
ρ ρ ρ= +
= += +
LPCE (Seo & Moon, JCP, 2006)
Subtracting INS from CNS
Linearization and suppressing the generation and evolution of vortical component on the acoustic field.
Need to use high (6th) order schemes to accurately model sound propagation
0' ( ) ' ( ') 0U u
tρ ρ ρ∂
+ ⋅∇ + ∇⋅ =∂
0
' 1( ' ) ' 0u u pt
Uρ
∂+∇ ⋅ + ∇ =
∂
' ( ) ' ( ') ( ' )p p u u Dt
U P PDt
Pγ∂+ ⋅∇ + ∇⋅ + ⋅∇ = −
∂St
PS
D(d
B)
0.2 0.4 0.6 0.8 1 1.20
20
40
60
80
100
120
Noise generated by turbulent flow over a circular cylinder at ReD = 46000 , M = 0.21
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Immersed Boundary Method for Immersed Boundary Method for LPCE LPCE ( Approximating Polynomial Method)( Approximating Polynomial Method)
R
Body point (x0,y0,z0)
Ghost point (x’ 1,y’ 1,z’ 1)
Data points (x’m,y’m,z’m)
0 0 0( ', ', ') ( ', ', ') ( ') ( ') ( ') ,
N N Ni j k
ijki j k
x y z x y z c x y z i j k Nφ= = =
Φ = + + ≤∑∑∑
NNNumber of Number of
coefficientscoefficients
2D2D 3D3D
11 33 4422 66 101033 1010 202044 1515 3535
[ ]22
1( ' , ' , ' ) ( ' , ' , ' )
M
m m m m m m mm
w x y z x y zε φ=
= Φ −∑
(H. Luo et al.)
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32t
p'
0 2 4 6 8 10-4.0E-05
0.0E+00
4.0E-05
8.0E-05
c
Benchmark: Sound scattering by Benchmark: Sound scattering by a Circular Cylindera Circular Cylinder
p'rms
0
30
60
90
120
150
18010-6 10-5
Directivity at r=5
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Acoustic Scattering from Complex GeometriesAcoustic Scattering from Complex Geometries
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y/D
∆p'
20 40 60 80-0.001
-0.0005
0
0.0005
0.001
34
DNS
Comparison with DNS
DNS : full compressible N-S Eqs. on a body-fitted O-grid
ViCar3D
carLPCE
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Phonation and Speech
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Sound in Complex Configurations
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Sound in Complex Configurations
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AcknowledgementsAcknowledgements
PostdocsPostdocs and Studentsand Students–– XudongXudong ZhengZheng, Jung, Jung--HeeHee SeoSeo, , QianQian XueXue, , LingxiaoLingxiao
ZhengZheng, , EhsanEhsan Aram, Aram, HaoxiangHaoxiang LuoLuo, , HaiboHaibo DongDong
CollaboratorsCollaborators–– Dr. Dr. FadyFady NajjarNajjar (LLNL), (LLNL), Prof. George LauderProf. George Lauder (Harvard (Harvard
U.), Prof. James U.), Prof. James TangorraTangorra (Drexel U.), Prof. Ian Hunter (Drexel U.), Prof. Ian Hunter (MIT), (MIT), Prof. Frank FishProf. Frank Fish (Westchester University), Prof. (Westchester University), Prof. Ryan Ryan VallanceVallance (GWU), Prof. James Hahn (GWU), Dr. (GWU), Prof. James Hahn (GWU), Dr. Steve Steve BielamowiczBielamowicz, , Prof. Tyson Hedrick (UNC)Prof. Tyson Hedrick (UNC)
SponsorsSponsors–– AFOSR, NIH, NSF, USA Swimming, NASAAFOSR, NIH, NSF, USA Swimming, NASA
Questions?Questions?