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Fluid and Deformable-Structure Interactions in Bio-Mechanical Systems and Micro-Air Vehicles Lucy Zhang Department of Mechanical, Aerospace, and Nuclear Engineering Rensselaer Polytechnic Institute Troy, NY

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Page 1: Seminar GE

Fluid and Deformable-Structure Interactions in Bio-Mechanical Systems and Micro-Air Vehicles

Lucy Zhang

Department of Mechanical, Aerospace, and Nuclear Engineering

Rensselaer Polytechnic InstituteTroy, NY

Page 2: Seminar GE

log (m)

-2

-7

-6 -5

-4 -3

-8

biomaterial

Multiscale bio-mechanical systems

platelet

protein

red blood cell

vesselheart

Fluid-structure interactions at all scales

Page 3: Seminar GE

Numerical methods for fluid-structure interactions

• Commercial softwares (ABAQUS, ANSYS, FLUENT…)• Explicit coupling technique - generate numerical instabilities (oscillations), diverged solutions

• Arbitrary Lagrangian Eulerian (ALE)• limited to small mesh deformations• requires frequent re-meshing or mesh update

Page 4: Seminar GE

QuickTime™ and aYUV420 codec decompressor

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• Goals:• accurate (interpolations at the fluid-structure interface)• efficient (less/no mesh updating required)• flexible (deformable and rigid structures, boundary conditions)• extensibility (multi-phase flows, various applications)

• Immersed Boundary Method (Peskin) - flexible solid immersed in fluid• structures are modeled with elastic fibers• finite different fluid solver with uniform grid

Page 5: Seminar GE

Immersed finite element method (IFEM): Fluid-deformable structure interaction

t=0

Assumptions:

• No-slip boundary condition at the fluid-solid interface• Solid is completely immersed in the fluid• Fluid is everywhere in the domain

solid

t = t1

solid

Page 6: Seminar GE

Equations of motion

ext,d

dijij

i ftv

+=σρ

Principle of virtual work:0

dd ext

, =⎟⎠⎞⎜⎝

⎛ −−∫Ω ijiji

i ftvv σρδ

1 2 3

ssis

isif

iif

i dt

vvdtvvd

tvv

ssΩΩΩ

ΩΩΩ δδ

δδ

δδ ρδρδρδ ∫∫∫ +−1

ssjiji

sfjiji

fjiji ss

dvdvdv ΩΩΩΩΩΩ ∫∫∫ +− ,,, σδσδσδ2

si

si

si

fii

fi dgvdgvdgv

ssΩΩΩ

ΩΩΩρδρδρδ ∫∫∫ +− 3

Ω Ωs

Page 7: Seminar GE

Ω

IFEM continued …

f iFSI ,s = ρ f − ρ s( )

dv is

dt+ σ ij, j

s −σ ij, jf + ρ s − ρ f( )giSolid: in Ωs

ρ f (∂v i

∂t+ v jv i, j ) = σ ij, j

f + f iFSI(x,t)

v i,i = 0

fluid: in Ω

Overlapping

Ωs

Page 8: Seminar GE

Interpolations at the interface

∫ −=Ω

Ωd)(),(),( sFSI,FSI ss tt xxXfxf δ

vs(Xs,t) = v(x,t)δ(x − x s)dΩΩ∫

Force distribution

Velocity interpolation

solid nodeInfluence domainSurrounding fluid nodes

Uniform spacing

Page 9: Seminar GE

Read solid & fluid Geometries

Apply initial conditions

Distribute F onto the fluidFFSI,s -> FFSI Update solids positions

dsolid=Vsolid*dt

Interpolate vfluid onto solids Vsolid

vfluid->Vsolid

Fluid analysis (N-S)Solve for vfluid

Structure analysis Solve for FFSI,s

IFEM Algorithm

Page 10: Seminar GE

Validations

Flow past a cylinder

Soft disk falling in a channel

Leaflet driven by fluid flow

3 rigid spheres dropping in a channel

Page 11: Seminar GE

Particle (elastic):

Density= 3,000 kg/m3

Young modulus: E = 1,000 N/m2

Poisson ratio: 0.3

Gravity: 9.81 m/s2

Particle mesh: 447 Nodes and 414 Elements

Fluid:

Tube diameter, D = 4d =2 cm

Tube height, H = 10 cm

Particle diameter, d = 0.5 cm

Density= 1,000 kg/m3

Fluid viscosity = 0.1 N/s.m2

Fluid initially at rest

Fluid mesh: 2121 Nodes and 2000 Elements

A soft disk falling in a viscous fluid

Page 12: Seminar GE

Fluid recirculation around the soft disk

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Page 13: Seminar GE

Pressure distribution

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Page 14: Seminar GE

yyσ xyσ

t = 0.0 s

t = 1.1 s

t = 2.2 s

t = 3.3 s

t = 4.35 s

xxσ

Stress distribution on the soft disk

Page 15: Seminar GE

Comparison between the soft sphere and the analytical solution of a same-sized rigid sphere

Terminal velocity of the soft disk

ut =ρ s − ρ( )gr2

4μln L

r ⎛ ⎝ ⎜

⎞ ⎠ ⎟− 0.9157 +1.7244 r

L ⎛ ⎝ ⎜

⎞ ⎠ ⎟2

−1.7302 rL ⎛ ⎝ ⎜

⎞ ⎠ ⎟4 ⎛

⎝ ⎜ ⎜

⎠ ⎟ ⎟

Page 16: Seminar GE

3 rigid spheres dropping in a tube

QuickTime™ and aMicrosoft Video 1 decompressorare needed to see this picture.

Page 17: Seminar GE

3 rigid spheres dropping in a tube

Page 18: Seminar GE

• Why is it unique?

• fluid- deformable structure interactions

• two-way coupling, higher order interpolation function

• Limitations?

• time step constraint

• rigid solid case

• Possible expansions?

• compressible system

• multiphase flow

• Usefulness?

• numerous applications!

Page 19: Seminar GE

Use numerical methods to understand and study cardiovascular diseases.

Find non-invasive means to predict physical behaviors and seek remedies for diseases Simulate the responses of blood flow (pressure and velocities) under different physiologic conditions. Compare our results (qualitatively) with published clinical data and analyze the results.

Page 20: Seminar GE

Biomechanical applications

Red Blood Cell aggregationHeart modeling - left atrium

Deployment of angioplasty stent

Venous valves

Large deformation (flexible)

Page 21: Seminar GE

Why heart?

Cardiovascular diseases are one of the leading causes of death in the western world.

Cardiovascular diseases (CVD) accounted for 38.0 percent of all deaths or 1 of every 2.6 deaths in the United States in 2002. It accounts for nearly 25% of the deaths in the word.

In 2005 the estimated direct and indirect cost of CVD is$393.5 billion.

Page 22: Seminar GE

Cardiovascular system

D: The oxygen-poor blood (blue) from the superior vena cava and inferior vena cava fills the right atrium.

E: The oxygen-poor blood in the right atrium fills the right ventricle via tricuspid valve.

F: The right ventricle contracts and sends the oxygen-poor blood via pulmonary valve and pulmonary artery to the pulmonary circulation.

A: The oxygen-rich blood (red) from the pulmonary vein fills the left atrium.

B: The oxygen-rich blood in the left atrium fills the left ventricle via the mitra valve.

C: The left ventricle contracts and sends the oxygen-rich blood via aortic valve and aorta to the systemic circulation.

AF

D

E

CB

Page 23: Seminar GE

During Atrial Fibrillation (a particular form of an irregular or abnormal heartbeat):

The left atrium does not contract effectively and is not able to empty efficiently.

Sluggish blood flow may come inside the atrium.

Blood clots may form inside the atrium. 

Blood clots may break up

Result in embolism.

Result in stroke.

Atrial fibrillation and blood flow

Without blood clots

with a blood clot

Left atrial appendage

Page 24: Seminar GE

From Schwartzman D., Lacomis J., and Wigginton W.G., Characterization of left atrium and distal pulmonary vein morphology using

multidimensional computed tomography. Journal of the American College of Cardiology, 2003.

41(8): p. 1349-1357Ernst G., et al., Morphology of the

left atrial appendage. The Anatomical Record, 1995. 242: p.

553-561. Left atrium

Left atrial appendage

Pulmonary veins

Left atrium geometry

77mm

28mm

20mm

17mm 56mm

Page 25: Seminar GE

During diastole (relaxes, 0.06s < t < 0.43s) , no flow through the mitral valve (v=0)

During systole (contracts, 0.43s < t < 1.06s), blood flow is allowed through the mitral valve (free flow)

Blood is assumed to be Newtonian fluid, homogenous and incompressible. Maximum inlet velocity: 45 cm/sBlood density: 1055 kg/m3

Blood viscosity: 3.5X10-3 N/s.m2

Fluid mesh: 28,212Nodes, 163,662 ElementsSolid mesh: 12,292 Nodes, 36,427 Elements

Left atrium with pulmonary veins

Klein AL and Tajik AJ. Doppler assessment of pulmonary venous flow in healthy subjects and in patients with heart disease. Journal of the American Society of Echocardiography, 1991, Vol.4, pp.379-392.

Page 26: Seminar GE

QuickTime™ and aMotion JPEG OpenDML decompressor

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Pressure distribution at the center of the atrium during a diastole and systole cycle

Transmitral velocity during diastole

Left atrium with appendage

Page 27: Seminar GE

Rigid wall

QuickTime™ and aH.264 decompressor

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Page 28: Seminar GE

Pressure distribution at the

center of the atrium during

one cardiac cycle

Transmitral velocity during

one cardiac cycle

Kuecherer H.F., Muhiudeen I.A., Kusumoto F.M., Lee E., Moulinier L.E., Cahalan M.K. and Schiller N.B., Estimation of

mean left atrial pressure from transesophageal pulsed Doppler echocardiography of pulmonary venous flow

Circulation, 1990, Vol 82, 1127-1139

E

A

Left atrium (comparison with clinical data)

5

Pressure (mm hg)

2 Time (s)

1.510

Page 29: Seminar GE

Transmitral velocity during one cardiac cycle (with and without the appendage)

Velocity inside the appendage during one cardiac cycle

Influence of the appendage

Page 30: Seminar GE

Left atrium geometry

Courtesy of Dr. A. CRISTOFORETTI,[email protected]

University of Trento, Italia

G. Nollo, A. Cristoforetti, L. Faes, A. Centonze, M. Del Greco, R. Antolini, F. Ravelli: 'Registration and Fusion of Segmented Left Atrium CT Images with CARTO Electrical Maps for the Ablative Treatment of Atrial Fibrillation', Computers in Cardiology 2004, volume 31, 345-348;

Pulmonary veins

Pulmonary veins

Left atrium

Left atrial appendage

Pulmonary veins

Pulmonary veins

Mitral valveLeft

atriumBlood clots

Page 31: Seminar GE

Red blood cells and blood

RBC FEM RBC model

From Dennis Kunkel at http://www.denniskunkel.com/

10ìm2ìm

Property of membrane•Thickness of RBC membrane: 7.5 to 10 nm•Density of blood in 45% of hematocrit: 1.07 g/ml•Dilation modulus: 500 dyn/cm•Shear modulus for RBC membrane: 4.2*10-3dyn/cm•Bending modulus: 1.8*10-12 dyn/cm.

Property of inner cytoplasm •Incompressible Newtonian fluid

empirical function

Page 32: Seminar GE

The shear rate dependence of normal human blood viscoelasticity at 2 Hz and 22 °C (reproduced from http://www.vilastic.com/tech10.html)

Bulk aggregates Discrete cells Cell layers

Red blood cells and blood

Page 33: Seminar GE

Shear of a RBCs Aggregate

The shear of 4 RBCs at low shear rate

The RBCs rotates as a bulk

The shear of 4 RBCs at high shear rate

The RBCs are totally separated and arranged at parallel layers

The shear of 4 RBCs at medium shear rate

The RBCs are partially separated

RBC-RBC protein dynamic force is coupled with IFEM (NS Solver)C-Cf

QuickTime™ and aH.264 decompressor

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QuickTime™ and aH.264 decompressor

are needed to see this picture.QuickTime™ and aH.264 decompressor

are needed to see this picture.

Page 34: Seminar GE

Micro-air vehicles

QuickTime™ and aTIFF (Uncompressed) decompressor

are needed to see this picture.

http://www.fas.org/irp/program/collect/docs/image1.gif

three types of MAVs:1. airplane-like fixed wing model, 2. helicopter-like rotating wing model, 3. bird-or insect-like flapping wing model.

potential military and surveillance use

10-4

1

0-3

10-2

1

0-1

1

10

1

02

10

3

10

4

105

1

06

Gro

ss W

eigh

t (Lb

s)

Page 35: Seminar GE

MAVs

Features:• improved efficiency, • more lift, • high maneuverability,• reduced noise.

Loitering wings: high span and a large surface areaFast wings: a low wing span and a small areaFlying efficiently at high speed: small, perhaps, swept wings Flying at slow speed for long periods: long narrow wings

Page 36: Seminar GE
Page 37: Seminar GE

Bio-inspired flapping wings

muscle contraction

Page 38: Seminar GE

Acknowledgement

•Graduate students: • Mickael Gay, Yili Gu

• Collaborators: • Dr. Holger Salazar (Cardiology Department, Tulane University)• Dr. A. Cristoforetti (University of Trento, Italy)

• Funding agencies: NSF, NIH, Louisiana BOR

• Computing resources: •Center for Computational Sciences (CCS) - Tulane• SCOREC (RPI)

Page 39: Seminar GE
Page 40: Seminar GE

What can you do?

Page 41: Seminar GE

IFEM: Governing Equations

ρ s ∂2us

∂t 2

⎛ ⎝ ⎜

⎞ ⎠ ⎟−∇ ⋅σ s = f sur + ρ sg on Ωs

f = f sur (X)δ(x − X)dVΩ s

ρ f ∂v∂t

+ v ⋅∇v ⎛ ⎝ ⎜

⎞ ⎠ ⎟=∇ ⋅? + f on Ω

∇ ⋅v = 0

dX /dt = v(x)δ(x − X)dVΩ∫

Navier-Stokes equation for incompressible fluid

Governing equation of structure

Force distribution

Velocity interpolation

ΩsΩ

Page 42: Seminar GE

IFEM: Solid Force Calculationextsurint fffMa +=+

gf )(ext ρρ −= σVol

External Forces: External forces can be arbitrary forces from diverse force fields (e.g. gravity, buoyancy force, electro-magnetic fields).

g – acceleration due to gravity

VSs I

pqpqI dint ∫Ω ∂∂

=X

Internal Forces: hyperelastic material description (Mooney-Rivlin material).

S – 2nd Piola Kirchhoff stress tensor

ε - Green Lagrangian strain tensorTotal Lagrangian Formulation

Page 43: Seminar GE

ρ ∂v∂t

+ ρv ⋅∇v =∇ ⋅σ f + f FSI

∇ ⋅v = 0

Solve for velocity using the Navier-Stokes equation Eq. (III)

The interaction force fFSI,s is distributed to the fluid domain via RKPM delta function.

The fluid velocity is interpolated onto the solid domain via RKPM delta function

ΩsΩ

∫Ω Ω−= d)(),(),( sss tt xxxvXv φ

∫Ω Ω−= d)(),(),( sFSI,FSI ss tt xxXfxf φ

−Δρ ∂vs

∂t+ (∂σ s

∂x− ∂σ f

∂x) + Δρg

sΩin Ωin

),(FSI txf),(sFSI, tsXf

tt

ss

∂∂

≡∂∂ vu

2

2

The interaction force is calculated with Eq. (I)

sFSI,f

I.

IV.

III.

II.

),( txvP and v unknowns are solved

by minimizing residual vectors (derived from their

weak forms)

Distribution of interaction force

Insert this inhomogeneous fluid force field into the N-S eqn.

Update solid displacement with

solid velocity

IFEM Governing Equations

=sFSI,f

Page 44: Seminar GE

Red blood cell modelRBC

From Dennis Kunkel at http://www.denniskunkel.com/

2ìm

Shear rate dependence of normal human blood viscoelasticity at 2 Hz and 22 °C (reproduced from http://www.vilastic.com/tech10.html)

Bulk aggregates Discrete cells Cell layers

Page 45: Seminar GE

Venous Valve

Courtesy of H.F. Janssen, Texas Tech University.

QuickTime™ and aMicrosoft Video 1 decompressorare needed to see this picture.

QuickTime™ and aBMP decompressor

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• Site of deep venous thrombosis formation• Prevents retrograde venous flow (reflux) • Site of sluggish blood flow• Decreased fibrinolytic activity• Muscle contraction prevents venous stasis:

– Increases venous flow velocity– Compresses veins

• Immobilization promotes venous stasis

Page 46: Seminar GE

Venous Valve Simulation

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Page 47: Seminar GE

Venous Valve

Comparison between experiment and simulation at 4 different time steps

Page 48: Seminar GE
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Multi-resolution analysis

⎟⎟⎠⎞

⎜⎜⎝⎛

Δ−

Δ=−

j

j

jja xa

xxxa

xx φφ 1)(

• Window function with a dilation parameter:

∑=

Δ−Φ==NNP

jjjaja

Ra xxxxxuxuPxu1

);()()()(

• Projection operator for the scale a

a: dilation parameter

• Wavelet function:);();();( 22 jajaja xxxxxxxxx −Φ−−Φ=−ψ

• Complementary projection operator:

∑=

Δ−=NNP

jjjaja xxxxxuxuQ

122 );()()( ψ

)()()( 22 xuQxuPxuP aaa +=low scale + high scale