A Coupling Interface Method for Elliptic Interface ProblemsDirichlet or Neumann boundary condition...
Transcript of A Coupling Interface Method for Elliptic Interface ProblemsDirichlet or Neumann boundary condition...
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An Augmented Coupling Interface Method for
Elliptic Interface ProblemsI-Liang Chern
National Taiwan University
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Goal
Propose a coupling interface method to solve the above elliptic interface problems.
Three applications: Computing electrostatic potential for Macromolecule in solvent Simulation of Tumor growthComputing surface plasmon mode at nano scale
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Collaborators
Chieh-Cheng Chang: Inst. of Applied Mechanics, National Taiwan Univ.Ruey-Lin Chern, Inst. Of Applied Mechanics, National Taiwan Univ.Yu-Chen Shu: Center for Research on Applied Sciences, Academia SinicaHow-Chih Lee, Math, National Taiwan Univ.Xian-Wen Dong, Math, National Taiwan Univ.
Ref. Chern and Shu, J. Comp. Phys. 2007Chang, Shu and Chern, Phys. Rev. B 2008
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Elliptic Interface Problems
ε and u are discontinuous,
f is singular across Γ
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Dielectric coefficients
Vacuum: 1Air :1-2Silicon: 12-13Water: 80Metal:
ε
610−
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Elliptic irregular domain problems
Poisson equation
Dirichlet or Neumann boundary condition
can be quite general and complex.
in u fΔ = Ω
Ω
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Biomolecule in solvent: Poisson-Boltzmann Equation
N. Baker, M. Holst, and F. Wang, Adaptive multilevel finite element solution of the Poisson-Boltzmann equation II: refinement at solvent accessible surfaces in biomolecular systems. J. Comput. Chem., 21 (2000), pp. 1343-1352. (Paper at Wiley)
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Biomolecule in solventPoisson-Boltzmann model
Macromolecule: 50 AHydrogen layer: 1.5 – 3AMolecule surface: thinDielectric constants:
2 inside molecule80 in water
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Tumor growth simulation (free boundary)(Lowengrub et al)
pressure :nutrient :
pΓ
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T=6 T=6 T=3
T=6 T=6
Initial condition: R=2.
Bifurcation of tumor growthT=6
(growth rate/adhersive force), A(apoptosis)G
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Surface plasmonsSurface plasmons are surface electromagnetic waves that propagate parallel along a metal/dielectric (or metal/vacuum) interface. E field excites electron motion on metal surfaceFields decay exponentially from the interface: surface evanescent waves.
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Surface plasmon
Macroscopic Maxwell Equation
0
2
0 )(1)(
μμ
ωωωω
εωετ
=
⎟⎟⎠
⎞⎜⎜⎝
⎛
+−=
ip0
0
t
t
DBE BH D
∇⋅ =⎧⎪∇⋅ =⎪⎨∇× = −⎪⎪∇× =⎩
D EB H
εμ
==
[ ][ ] 0
0condition Interface
=⋅=⋅
tHtE
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Plasma frequency
Quoted from Ordal et al., Applied Optics, 1985, Volume 24, pp.4493~4499
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Optical communication frequency
A goal of nanotechnology: fabrication of nanoscale photonic circuitsoperating at optical frequencies. Faster and Smaller devices.
Quoted from Jorg Saxler 2003
13
6
10
,10)(
=
−=
ω
ωεm
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Quadratic Eigenvalue problem for k:
2
2
0
0z z
z z
E E
H H
⎧∇ +Λ =⎪⎨∇ +Λ =⎪⎩
[ ] [ ] 0z zE H= =
z z
z z
kE H
kH E
εω
μω
⎡ ⎤ ⎡ ⎤∇ ⋅ = − ∇ ⋅⎢ ⎥ ⎢ ⎥Λ Λ⎣ ⎦ ⎣ ⎦⎡ ⎤ ⎡ ⎤∇ ⋅ = ∇ ⋅⎢ ⎥ ⎢ ⎥Λ Λ⎣ ⎦ ⎣ ⎦
n s
n s
( ) ( ) ( )
( ) ( ) ( )
, ,
, ,
x y
x y
i k L k Lz z
i k L k Lz z
E x L y L E x y e
H x L y L H x y e
+
+
⎧ + + =⎪⎨⎪ + + =⎩
Interior: Interface conditions:
Boundary conditions:
2 2kω εμΛ = −
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Surface Plasmon:
EM wave are confined on surface.
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Elliptic Interface Problems
ε and u are discontinuous,
f is singular across Γ
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Three classes of approaches
Boundary integral approach
Finite element approach:
Finite Difference approach:Body-fitting approach Fixed underlying grid: more flexible for moving interface problems
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Regular Grid Methods for Solving Elliptic Interface Problems
Regularization approach (Tornberg-Engquist, 2003)Harmonic Averaging (Tikhonov-Samarskii, 1962)Immersed Boundary Method (IB Method) (Peskin, 1974)Phase field method
Dimension un-splitting approachImmersed Interface Method (IIM) (LeVeque-Li, 1994)Maximum Principle Preserving IIM (MIIM) (Li-Ito, 2001)Fast iterative IIM (FIIM) (Li, 1998)
Dimension splitting approachGhost Fluid Method (Fedkiw et al., 1999, Liu et al. 2000)Decomposed Immersed Interface Method (DIIM) (Berthelsen, 2004)Matched Interface and Boundary Method (MIB) (YC Zhou et al., 2006)Coupling interface method (CIM) (Chern and Shu 2007)
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Coupling Interface Method (CIM)
CIMCIM1 (first order)CIM2 (2nd order)Hybrid CIM (CIM1 + CIM2) for complex interface problems
Augmented CIMAuxiliary variables on interfaces
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Numerical Issues for dealing with interface problems
Accuracy: second-order in maximum norm.
Simplicity: easy to derive and program.
Stability: nice stencil coefficients for linear solvers.
Robustness: capable to handle complex interfaces.
Speed: linear computational complexity
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CIM outline
1d: CIM1, CIM22d: CIM22d: Augmented CIMd dimensionHybrid CIMNumerical validation
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CIM1: one dimension
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CIM2: One dimension
Quadratic approximation and match two grid data on each side
Match two jump conditions
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CIM2: One dimension
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CIM2: 2 dimensions
Coupling Interface Method
Stencil at a normal on-front points (bullet) (8 points stencil)
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CIM2 Case 1:
Coupling Interface Method
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CIM2 (Case 1):
Dimension splitting approach
Decomposition of jump condition
One side interpolation
Coupling Interface Method
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CIM2 (Case 1):
Bounded by 1 and ε+/ε-.
Coupling Interface Method
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CIM2 (Case 2):
Coupling Interface Method
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Dimension splitting approach
Decomposition of jump conditions
One-side interpolation
CIM2 (Case 2):
Ω-
Ω+
Coupling Interface Method
The second order derivatives are coupled by jump conditions
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CIM2 (Case 2): results a coupling matrix
Theorem: det(M) is positive when local curvature is zero or h is small
Coupling Interface Method
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Augmented CIM
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Augmented CIM
Auxiliary interfacial variables are distributed on the interface almost uniformly.
The jump information at the intersections of grid line and interface is expressed in terms of interfacial variables at nearby interfacial grid.
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Apply 1-d method in x- and y-directions
( ) ( )R
RPR
RPRP yx
EyyxExx
xE
xE
⎥⎦
⎤⎢⎣
⎡∂∂
∂−+⎥
⎦
⎤⎢⎣
⎡∂∂
−+⎥⎦⎤
⎢⎣⎡
∂∂
=⎥⎦⎤
⎢⎣⎡
∂∂ 2
2
2
εεεε
2
, , , 1: 2,2
2
, , , , 1: 22
( ,[ ] )
( ,[ ] )
i j i j x i i j x P
i j i j y i j j y Q
E L E uxE L E u
y
ε
ε
− +
− +
∂=
∂∂
=∂
( ) ( )2 2
2Q R P RRQ R R
E E E Ey y x xy x y x y
ε ε ε ε⎡ ⎤ ⎡ ⎤⎡ ⎤∂ ∂ ∂ ∂⎡ ⎤= + − + −⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢ ⎥∂ ∂ ∂ ∂ ∂⎣ ⎦⎣ ⎦ ⎣ ⎦ ⎣ ⎦
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Resulting scheme
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CIM1: d dimensions
Dimension splitting approach
Decomposition of jump conditions
One-side interpolation
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CIM2: d dimensions
Dimension splitting approach
Decomposition of jump conditions
One-side interpolation
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CIM2: d dimensions, coupling matrix
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Complex interface problemsClassification of grid
Interior points (bullet) (contral finite difference)
Nearest neighbors are in the same side
On-front points (circle and box)
Normal (circle) (CIM2).Exceptional (box) (CIM1).
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Classification of grids for complex interface (number of grids)
Interior grids: Normal on-fronts (CIM2):Exceptional (CIM1):
The resulting scheme is still 2nd order
( )dO h−
1( )dO h −
(1)O
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Numerical Validation
Stability of CIM2 in 1dOrientation error of CIM2 in 2dConvergence tests of CIM1Comparison results (CIM2)Complex interfaces results (Hybrid CIM)
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Stability Issue of CIM2 in 1-dLet ( , ) be the resulting matrix.A Nα
Insensitive to the location of the interface in a cell.
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Orientation error from CIM2 is small
Insensitive to the orientation of the interface.
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Convergence tests for CIM1: interfaces
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Convergence of CIM1 (2) (order 1.3)log log plot of error versus N−
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Example 5 (for CIM2)
1000,10,1=b
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Example 5, figures
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Example 5 (for CIM2)
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Example 5 (CIM2)
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Example 5 (CIM2)
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Comparison results
Second order for u and its gradients in maximum norm for CIM2
Insensitive to the contrast of epsilon
Less absolute error despite of using smallersize of stencil
Linear computational complexity
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Hybrid CIM
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Number of exceptional points O(1) in general
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Convergence of hybrid CIM (order 1.8)
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Hybrid CIM
Capable to handle complex interface problems in three dimensions
Produce less absolute error than FIIM.
Second order accuracy due to number of exceptional points is O(1) in mostapplications.
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Some applications
Find electrostatic potential for macromolecule in solvent
Tumor growth simulation
Finding dispersion relation for surface plasmonic wave propagation
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Biomolecule in solvent: Poisson-Boltzmann Equation
N. Baker, M. Holst, and F. Wang, Adaptive multilevel finite element solution of the Poisson-Boltzmann equation II: refinement at solvent accessible surfaces in biomolecular systems. J. Comput. Chem., 21 (2000), pp. 1343-1352. (Paper at Wiley)
u
u
ee−
−
:ondistributiion negative :ondistributiion positive
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Poisson-Boltzmann equation
=K
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Numerical procedure
Construction of molecular surface (by MSMS)Treatment of singular charges
Nonlinear iteration by damped Newton’s method for the perturbed equationCoupling interface method to solve elliptic interface problemAlgebraic multigrid for solving linear systems
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Construction of molecular surface: MSMS
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Treatment of Singularity
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Damped Newton’s method
Ref. Holst
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Numerical Validation—Artificial molecule
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Numerical Validation
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Hydrophobic protein (PDB ID: 1 crn)
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Hydrophilic protein (PDB ID: 1DGN)
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Summary of computing Poisson-Boltzmann equation
Ingredients: CIM + AMG + damped Newton’s iterationSecond order accuracy for potential and electric field for molecules with smooth surfaces3-4 Newton’s iterations only
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Tumor growth Simulation
Lowengrub et al.
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Tumor growth model (1)
2
Assume the tumor depends on only one kind of nutrient .The governing equation of is
,
where ( ) .: the diffusion coeficient. ( ) : blood-tissue transfer.: nutrient con
B B
B B
Dt
D
σ
σ
σσ
σ σ
λ σ σ λσ
λ σ σλσ
∂= ∇ +Γ
∂Γ=− − −
−sumption of cells.
Nutrient model
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Cell evolution
P cells
(proliferating)
D cells(dead)
Q cells(quiescent)
Birth
Apoptosis
starvation
Cell death
Degrade
recovery
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Tumor growth model (2)
Then the governing equations for P, Q and D are
P ( ) ( ( ) ( ) ( )) ( )t
( ) ( ) [ ( ) ( )]t
( ) ( ) ( ) .t
Since P+Q+D=1, in fact we have only two indepen
B Q A P
Q P D
A D R
Pv K K K P K Q
Q Qv K P K K Q
D Dv K P K Q K D
σ σ σ σ
σ σ σ
σ σ
∂+∇ ⋅ = − − +
∂∂
+∇ ⋅ = − +∂∂
+∇ ⋅ = − −∂
v
v
v
dent equations.Summing three equations together,
( ) (( ) ) ( ) .B RP Q D P Q R v v K P K D
tσ∂ + +
+∇ ⋅ + + = ∇ ⋅ = −∂
v v
Reaction diffusion model for cell populations
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Tumor growth model (3)
Momentum equation: Darcy’s law
Boundary condition:p vα−∇ =
r
p γκ=
is the mean curvature of the interfaceκ
Free boundary problem
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Quasi-steady approximation
Assume Q = 0 (sufficient nutrient available)D is digested very fast 1>>RK
0,0,1 ≈=≈ DQP
( ) ( ) ( ) PKKDKPKv ABRB ][ σσσ −≈−=⋅∇
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Quasi-steady approximationfor tumor growth
pressure theis nutient theis
pσ
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Dimensionless formulation (Lowengrub et al)
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Numerical procedure
Level set method for interface propagationWENO5 + RK3 for interface propagationLeast square method for velocity extensionCoupling interface method for elliptic problems on arbitrary domain
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Numerical Validation (1)
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Numerical Validation (2)
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Numerical Validation (3)
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T=6 T=6 T=3
T=6 T=6
Initial condition: R=2.
Bifurcation of tumor growth
T=6
(growth rate/adhersive force), A(apoptosis)G
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Surface plasmonsSurface plasmons are surface electromagnetic waves that propagate parallel along a metal/dielectric (or metal/vacuum) interface. E field excites electron motion on metal surface
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Drude model
0)( =⋅∇ Eε
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Plasma frequency
Quoted from Ordal et al., Applied Optics, 1985, Volume 24, pp.4493~4499
=γ
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Drude model for gold
Quoted from Jorg Saxler 2003
Drude model is good approximation for 1410<pω
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Optical communication frequency
A goal of nanotechnology: fabrication of nanoscale photonic circuitsoperating at optical frequencies. Faster and Smaller devices.
Quoted from Jorg Saxler 2003
13
6
10
,10)(
=
−=
ω
ωεm
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Wave propagation in metal
pω
Region of attenuation Region of propagation
0.5 1.5 2.01.0
1.0
-1.0
( )ε ω
p
ωω
is the frequency of collective oscillations of the electron gas.
Drude modelfor permittivity
( ) 2
2
1ωω
ωε p−=
D = εE
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Maxwell equation in matter
Macroscopic Maxwell Equation
0
2
0 )(1)(
μμ
γωωω
εωε
=
⎟⎟⎠
⎞⎜⎜⎝
⎛
+−=
ip0
0
t
t
DBE BH D
∇⋅ =⎧⎪∇⋅ =⎪⎨∇× = −⎪⎪∇× =⎩
D EB H
εμ
==
[ ][ ] 0
0condition Interface
=⋅=⋅
tHtE
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Dispersion relation: Bulk case
)(00 ),(),( tkzieHEHE ω−=
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ε + : dielectric: metal( )0ε − <
ε +
z
y
x
ε −
Dispersion relation: 1 interfaceSurface Plasmon modes
( )
( )2
22
222
⎟⎠⎞
⎜⎝⎛=+
⎟⎠⎞
⎜⎝⎛=+
ckk
ckk
mm
dd
ωε
ωε
mdieeHEHE tiikzyiki
,),(),( 00
== − ω
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Dispersion relation: 1 interface case
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Dispersion relation: Slab -1
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Slab-20 1 0 0 2 0 0 3 0 0 4 0 0 5 0 0 6 0 0 7 0 0 8 0 0
-0 . 2
-0 . 1 5
-0 . 1
-0 . 0 5
0
0 . 0 5
0 . 1
0 . 1 5
0 . 2
0 1 0 0 2 0 0 3 0 0 4 0 0 5 0 0 6 0 0 7 0 0 8 0 00
0 . 0 2
0 . 0 4
0 . 0 6
0 . 0 8
0 . 1
0 . 1 2
0 . 1 4
0 . 1 6
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Surface plasmons
From Wikipedia, the free encyclopedia
The excitation of surface plasmons by light is denoted as a surface plasmon resonance (SPR) for planar surfaces or localized surface plasmon resonance (LSPR) for nanometer-sized metallic structures.Since the wave is on the boundary of the metal and the external medium (air or water for example), these oscillations are very sensitive to any change of this boundary, such as the adsorption of molecules to the metal surface.
This phenomenon is the basis of many standard tools for measuring adsorption of material onto planar metal (typically gold and silver) surfaces or onto the surface of metal nanoparticles. It is behind many color based biosensorapplications and different lab-on-a-chip sensors.
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Surface plasmon
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Wave propagation in periodic nanostructure
xy
z
x y
z
Metal-dielectric materials
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Surface Plasmon
EM wave are confined on surface.
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Goal: study band structure
Signal propagation via surface plasmonicwavesEnergy absorbing problem
( )k k ω=
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Waveguide: homogeneous in z direction( ) ( )
( ) ( )
, , ,
, ,
i kz tx y z
i kz tx y z
E E E E e
H H H H e
ω
ω
−
−
=
=
z zx
z zy
z zx
z zy
E HiE kx y
E HiE ky x
H EiH kx y
H EiH ky x
ωμ
ωμ
ωε
ωε
⎧ ∂ ∂⎛ ⎞= +⎪ ⎜ ⎟Λ ∂ ∂⎝ ⎠⎪
⎪ ∂ ∂⎛ ⎞= −⎪ ⎜ ⎟Λ ∂ ∂⎪ ⎝ ⎠
⎨∂ ∂⎛ ⎞⎪ = −⎜ ⎟⎪ Λ ∂ ∂⎝ ⎠⎪∂ ∂⎪ ⎛ ⎞
= +⎜ ⎟⎪ Λ ∂ ∂⎝ ⎠⎩
2 2kω εμΛ = −
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Reduced equations for
2 22 2
2 22 2
z zz
z zz
E k H E
H k E H
ε εω
μ μω
⎧ ∇ ∇⎛ ⎞ ⎛ ⎞∇ ⋅ +∇ × = −⎜ ⎟ ⎜ ⎟⎪ Λ Λ⎪ ⎝ ⎠ ⎝ ⎠⎨
∇ ∇⎛ ⎞ ⎛ ⎞⎪∇ ⋅ +∇ × = −⎜ ⎟ ⎜ ⎟⎪ Λ Λ⎝ ⎠ ⎝ ⎠⎩
From Faraday’s Law and Ampere’s Law(curl equations)
⎟⎟⎠
⎞⎜⎜⎝
⎛∂∂
∂∂
=∇yx
,2
( , )z zE H
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Interface Conditions[ ] [ ][ ][ ]
0, 0
0
0
1
1
z
z
z z
z z
E T H T
E
H
E k H
H k E
εω
μω
⋅ = ⋅ =
=⎧⎪
=⎪⎪⎪ ⎡ ⎤ ⎡ ⎤⇒ ⎨ ∇ ⋅ = − ∇ ⋅⎢ ⎥ ⎢ ⎥Λ Λ⎣ ⎦ ⎣ ⎦⎪⎪ ⎡ ⎤ ⎡ ⎤⎪ ∇ ⋅ = ∇ ⋅⎢ ⎥ ⎢ ⎥Λ Λ⎪ ⎣ ⎦ ⎣ ⎦⎩
n s
n s
Continuous along the tangential directionns
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Boundary Condition
( ) ( ) ( )
( ) ( ) ( )
, ,
, ,
x y
x y
i k L k Lz z
i k L k Lz z
E x L y L E x y e
H x L y L H x y e
+
+
⎧ + + =⎪⎨⎪ + + =⎩
Bloch Boundary Condition: Suppose the domain is [ ] [ ]0,0, L L×
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Quadratic Eigenvalue problem for k:
2
2
0
0z z
z z
E E
H H
⎧∇ +Λ =⎪⎨∇ +Λ =⎪⎩
[ ] [ ] 0z zE H= =
z z
z z
kE H
kH E
εω
μω
⎡ ⎤ ⎡ ⎤∇ ⋅ = − ∇ ⋅⎢ ⎥ ⎢ ⎥Λ Λ⎣ ⎦ ⎣ ⎦⎡ ⎤ ⎡ ⎤∇ ⋅ = ∇ ⋅⎢ ⎥ ⎢ ⎥Λ Λ⎣ ⎦ ⎣ ⎦
n s
n s
( ) ( ) ( )
( ) ( ) ( )
, ,
, ,
x y
x y
i k L k Lz z
i k L k Lz z
E x L y L E x y e
H x L y L H x y e
+
+
⎧ + + =⎪⎨⎪ + + =⎩
Interior: Interface conditions:
Boundary conditions:
2 2kω εμΛ = −
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Ingredients of Numerical method
Interfacial operator: to reduce interface condition to a quadratic eigenvalue problem
Augmented Coupling interface method: to discretize the equation under Cartesian grid and interface condition under uniform interfacial grids.
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Interfacial operator:
z z
z z
kE H
kH E
εω
μω
⎡ ⎤ ⎡ ⎤∇ ⋅ = − ∇ ⋅⎢ ⎥ ⎢ ⎥Λ Λ⎣ ⎦ ⎣ ⎦⎡ ⎤ ⎡ ⎤∇ ⋅ = ∇ ⋅⎢ ⎥ ⎢ ⎥Λ Λ⎣ ⎦ ⎣ ⎦
n s
n s
2 2
2 2
E E E E H Hk kn n n n s s
H H H H E Ek kn n n n s s
ω ε ε μ μ ε ε ω ε μ ε μ
ω μ μ ε ε μ μ ω ε μ ε μ
+ − + − + −+ − − + + − − − + +
+ − + − + −+ − − + + − − − + +
⎧ ⎛ ⎞ ⎛ ⎞ ⎛ ⎞∂ ∂ ∂ ∂ ∂ ∂− = − − −⎪ ⎜ ⎟ ⎜ ⎟ ⎜ ⎟∂ ∂ ∂ ∂ ∂ ∂⎪ ⎝ ⎠ ⎝ ⎠ ⎝ ⎠
⎨⎛ ⎞ ⎛ ⎞ ⎛ ⎞∂ ∂ ∂ ∂ ∂ ∂⎪ − = − + −⎜ ⎟ ⎜ ⎟ ⎜ ⎟⎪ ∂ ∂ ∂ ∂ ∂ ∂⎝ ⎠ ⎝ ⎠ ⎝ ⎠⎩
Interfacial VariablesInterfacial operator
To form a quadratic eigenvalue problem for k.
C.C.Chang et.al. in 2005 (PRB 72, 205112)
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Augmented CIM
Auxiliary interfacial variables are distributed on the interface almost uniformly.
The jump information at the intersections of grid line and interface is expressed in terms of interfacial variables at nearby interfacial grid.
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Variables setup
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Apply 1-d method in x- and y-directions
( ) ( )R
RPR
RPRP yx
EyyxExx
xE
xE
⎥⎦
⎤⎢⎣
⎡∂∂
∂−+⎥
⎦
⎤⎢⎣
⎡∂∂
−+⎥⎦⎤
⎢⎣⎡
∂∂
=⎥⎦⎤
⎢⎣⎡
∂∂ 2
2
2
εεεε
2
, , , 1: 2,2
2
, , , , 1: 22
( ,[ ] )
( ,[ ] )
i j i j x i i j x P
i j i j y i j j y Q
E L E uxE L E u
y
ε
ε
− +
− +
∂=
∂∂
=∂
( ) ( )2 2
2Q R P RRQ R R
E E E Ey y x xy x y x y
ε ε ε ε⎡ ⎤ ⎡ ⎤⎡ ⎤∂ ∂ ∂ ∂⎡ ⎤= + − + −⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢ ⎥∂ ∂ ∂ ∂ ∂⎣ ⎦⎣ ⎦ ⎣ ⎦ ⎣ ⎦
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Resulting scheme
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Equations for interfacial variable
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Approximation
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Approximation
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Resulting linear combination
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Numerical Validation:1D test: parallel slab
0 100 200 300 400 500 600 700 800-0.2
-0.15
-0.1
-0.05
0
0.05
0.1
0.15
0.2
k = 6.481958
0 100 200 300 400 500 600 700 8000
0.02
0.04
0.06
0.08
0.1
0.12
0.14
0.16
k = 6.482042
Ez field
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Convergence result-1: 1d method, 2nd orderTM Mode. ω = 0.2, ω τ = 0width of metal / width of unit cell = 0.5
Insensitive to the relative location of the interface in a cell α
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Convergent order: 1d method, 2nd order
y = –2.1500x + 7.9918
Least square fit for errors from NxN runs, N=40,60,80,…,360
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Convergence Result-2: 1d method, 2nd order, different width of metal with damping
TM Mode. ω = 0.2, ω τ = 0.003, α = 0.5
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Numerical Validation:2d test: layer structure
Computational parameters of layer structureThe metal layer is located at the center of the unit cell and the width of metal layer is 0.4a. Target frequency is 0.7. There is no damping effect. Periodic boundary condition (kx = ky = 0) is applied at the cell boundary. N = 40, 80, 100, 120, 140, 160, 320, 400, 500, 600.
The exact solution is k = 1.888.
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Converge result for layer structure using 2d method
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Study of frequency band
Study signal propagation via plasmoniccrystal wave guide
Energy absorbing problem via plasmoniccrystal
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Study of frequency band: parallel slab
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Dispersion relation with different metal ratio
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Dispersion relation with different metal ratio
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Negative group velocity
For metal ratio > 0.5, the dispersion relation has negative group velocity. This means that energy can propagate in reverse direction.
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Skin depth: k larger, skin thinner
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Damping effect for SPPk larger, damp faster
( )
yellowcyan
redcka
ca
:)10,10[:)10,10[
:)10,0[2/Im
00296.02
23
36
6
−−
−−
−
∈
=
ππωτ
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Damping effect
The band lines closer to light line can travel longerFor surface plasmon, the larger k, the faster the waves decay
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Study of frequency band: parallel square
More SPP bands
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Damping effect
Waves corresponding to bands closer to light line survive longer.
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Computational parameters of eigenmodes of box
The box is located at the center of the unit cell and the metal is inside the box. Length of box/length of unit cell = 0.4. Target frequency is 0.7. There is no damping effect. Periodic boundary condition (kx = ky = 0) is applied at the cell boundary. N = 400.
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Upper(k=0.7000), Lower(k=0.7001), Eigenmodes of box
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Upper(k=0.7008), Lower(k=0.7161), Eigenmodes of box
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Study of frequency band: wavy slab
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Damping effect for wavy structure
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Signal propagation via plasmonic wave
As k increases, group velocity becomes slower, skin thickness becomes thinner, propagation length becomes shorterTransmission of signal via plasmonic wave is a trade-off problem between thinner thickness, faster group velocity and longer propagation lengthWavy structure provides more frequency for signal propagation
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Energy absorbing problem
Standing waves are concernedCurvature in wavy structure provides more frequency bands near k = 0 Wavy structure can absorb energy from wider range of frequency bands
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Conclusions
Augmented coupling interface method: 2nd orderInterfacial operator: reduce the problem to a standard quadratic eigenvalue problemCoupling interface method:
Cartesian grid in interior regionInterfacial grid on interfaceDimension-by-dimension approachDimensional coupling through solving coupling equation for second order derivatives
Wavy structure provides more frequency bands for signal propagation and energy absorption
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Summary
Propose coupling interface method for solving elliptic interface problems
CIM1, CIM2Augmented CIM
ApplicationsMacromolecule in solventTumor growth simulationComputing dispersion relation for surface plasmonat THz frequency ranges.
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Thank you for your attention!