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Implementation of perfectly matched layers in an arbitrary geometrical boundary for elastic wave

Implementation of perfectly matched layers in an arbitrary geometrical boundary for elastic wave
Implementation of perfectly matched layers in an arbitrary geometrical boundary for elastic wave

Geophys.J.Int.(2008)174,1029–1036doi:

10.1111/j.1365-246X.2008.03883.x

G J I S e i s m o l o g y

Implementation of perfectly matched layers in an arbitrary geometrical boundary for elastic wave modelling

Hongwei Gao and Jianfeng Zhang ?

State Key Laboratory of Lithosphere Evolution,Institute of Geology and Geophysics,Chinese Academy of Sciences,Beijing 100029,China.E-mail:zhangjf@https://www.doczj.com/doc/821273484.html,

Accepted 2008June 10.Received 2008April 4;in original form 2007November 25

S U M M A R Y

The perfectly matched layer (PML)absorbing boundary condition is incorporated into an irregular-grid elastic-wave modelling scheme,thus resulting in an irregular-grid PML method.We develop the irregular-grid PML method using the local coordinate system based PML splitting equations and integral formulation of the PML equations.The irregular-grid PML method is implemented under a discretization of triangular grid cells,which has the ability to absorb incident waves in arbitrary directions.This allows the PML absorbing layer to be imposed along arbitrary geometrical boundaries.As a result,the computational domain can be constructed with smaller nodes,for instance,to represent the 2-D half-space by a semi-circle rather than a rectangle.By using a smooth arti?cial boundary,the irregular-grid PML method can also avoid the special treatments to the corners,which lead to complex computer implementations in the conventional PML method.We implement the irregular-grid PML method in both 2-D elastic isotropic and anisotropic media.The numerical simulations of a VTI lamb’s problem,wave propagation in an isotropic elastic medium with curved surface and in a TTI medium demonstrate the good behaviour of the irregular-grid PML method.

Key words:Numerical solutions;Computational seismology;Wave propagation.

1I N T RO D U C T I O N

The perfectly matched layer (PML)absorbing boundary condi-tion has proven to be very ef?cient for modelling electromag-netic (B′e renger 1994),acoustic (Liu &Tao 1997)and elastic wave (Collino &Tsogka 2001)propagation in unbounded media.The PML method has been incorporated into a variety of wave propaga-tion algorithms,such as the velocity-stress ?nite-difference method of the ?rst-order system (Marcinkovich &Olsen 2003)and spectral-element method of the second-order system (Komatitsch &Tromp 2003;Festa &Vilotte 2005).The non-splitting PML method (Wang &Tang 2003)is also proposed.However,the current PML models are implemented in rectangular grids with vertical and horizontal edges.This means that the arti?cial boundaries have to be vertical and horizontal.Moreover,special treatments are required for han-dling the corners of the vertical and horizontal edges (Collino &Tsogka 2001;Marcinkovich &Olsen 2003).In practice,the arti-?cial boundaries can be constructed with arbitrary geometries as long as the zones of interest are enclosed.For example,we can take a semi-circle rather than a rectangle as the arti?cial boundaries in simulating the half-space (if a semi-circle PML absorbing layer is

?Corresponding author.

possible).This will result in an over 20per cent reduction of the

nodes in the numerical discretization.

The irregular-grid numerical schemes have proven to be useful in accounting for wave propagation across curved surface and in-terfaces as well as in using spatially varying sampling according to the local velocities (which will result in signi?cant reductions in the computational cost and in the storage requirements).However,it is not straightforward to incorporate the current PML methods with the irregular-grid schemes.An irregular-grid numerical tech-nique that can model elastic wave propagation in both 2-D and 3-D heterogeneous media,including surface and interface topographies,has been presented (Zhang &Liu 1999,2002;Gao &Zhang 2006).There it was called the grid method to distinguish it from the ?nite-element or ?nite-difference method.The grid method has also been extended to account for elastic wave propagation in media with high velocity contrasts (Zhang 2004a),in fractured media (Zhang 2005)and in mixed elastic/poroelastic (Zhang 2001)and ?uid/solid (Zhang 2004b)models.We therefore incorporate the PML model into the grid method,thus resulting in an irregular-grid PML model that has the ability to absorb incident waves in arbitrary directions.The irregular-grid PML method is developed using the local co-ordinate system based PML splitting equations and integral formu-lation of the PML equations under a discretization of triangular grid cells.The integral formulation is obtained following the grid method (Zhang &Liu 1999).The local coordinate system based PML

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splitting equations are formulated in a varying coordinate system whose one axis is always normal to the local arti?cial boundary.Due to the discretization of triangular grid cells and local coordinate sys-tem based splitting,the resulting PML model can be implemented along arbitrary geometrical boundaries on the irregular grids,in the absence of a certain decaying direction.This not only improves the grid method and other irregular-grid numerical schemes(e.g. Moczo1989;Zhang1997)in simulating unbounded media but allows the computational domain to be?exibly constructed,with smaller discretized nodes.The latter signi?cantly reduces the com-putational cost and storage requirements in the numerical simula-tions.Moreover,we can avoid the special treatments to the corners, as occurred in the conventional PML methods,by using a smoothed, curved arti?cial boundary.

Like the grid method,the numerical implementation of the irregular-grid PML method is simply completed by looping through all grid cells inside the PML region,based on the pre-calculated local geometrical coef?cients.This numerical scheme leads to a simpler computer implementation,in contrast to the current PML methods.Owing to that,the local geometrical coef?cients are picked up from a pre-calculated table in each time step,no extra computa-tional costs arise when the irregular-grid PML method is used.By extending the PML splitting equations to consider the anisotropic stiffness tensor,the resulting irregular-grid PML model can handle the anisotropic cases without any extra effort.In this paper,we im-plement the irregular-grid PML model in both2-D elastic isotropic and anisotropic media.

The paper is arranged as follows:?rst,we discuss the local co-ordinate system based PML splitting equations.Then,we present the integral formulation of the PML splitting equations,under a discretization of triangular grid cells,for the nodes inside the PML region and on the interface between the interior and the PML re-gion(we will call the interface the PML interface).Next,we review the numerical implementations when the irregular-grid PML model is incorporated into the grid method.Finally,we present exam-ples which demonstrate the irregular-grid PML method’s ability to absorb surface and body waves and to reduce the computational domain.

2P M L S P L I T T I N G E Q UAT I O N S

Following the PML splitting equations discussed in the conventional PML method(e.g.Collino&Tsogka2001),the local coordinate system based PML splitting equations in2-D anisotropic,elastic media are formulated,in a local coordinate system(x1,x2),with x1-axis being normal to the local arti?cial boundary,in terms of velocity and stress as follows:

ρ?v⊥i

?t

+ρd(x1)v⊥i=

?τi1

?x1

?v i

?t

=

?τi2

?x2

,(1)

?τ⊥i j

+d(x1)τ⊥i j=c i jl1?v l

1

,

?τ i j

=c i jl2

?v l

2

,(2)

τi j=τ⊥i j+τ i j,v i=v⊥i+v i,(3) where i,j,l=1,2,we assume the summation convention for repeated indices andρis the density,c ijln are the components of

a fourth-order elastic stiffness tensor,v i,v⊥

i and v

i

andτi j,τ⊥

i j

,

andτ

i j are,respectively,the velocity,split velocity components

and stress,split stress components that are de?ned in the local coordinate system(note thatτi j,etc.are symmetric),

superscript Figure1.Local mesh in the proximity of a curved arti?cial boundary.The

curve g-q-h denotes the arti?cial boundary(i.e.PML interface).A PML

absorbing layer is imposed along the arti?cial boundary.The width between

the upper and lower?gures is created for visualization.The triangles drawn

by solid lines are the grid cells.Coordinate system(x1,x2),for which

x1-axis coincides with the dotted-line segment,is related to grid cell pqk.

The dotted-line segment denotes the normal distance(i.e.a)from the centre

of grid cell pqk to the arti?cial boundary,which is used to compute the

damping factor at the centre of the grid cell.The damping factors become

zero at the centres of the grid cells in the upper?gure(i.e.outside the PML

absorbing layer).F z and F x denote the loads acting on interface1-g-5in

the vertical and horizontal directions,that is,in the total coordinate system.

The dashed lines link the centres of the grid cells,represented by circles,

and the midpoints of the edges of the grid cells.

⊥means that only the derivative perpendicular to the boundary is considered(superscript means that only the derivative parallel

to the boundary is considered)and d(x1)is the damping factor

that gradually increases from zero to a positive number along the

outward-directed normals(i.e.x1-axis).The term c ijln satis?es the

(Green)symmetry conditions,that is,c ijln=c jiln=c ijnl=c lnij.For isotropic cases,it is independent of the coordinate system and is

determined by two Lam′e parameters,that is,c ijln=λδi jδln+μ(δilδjn+δinδjl).In anisotropic cases,we obtain c ijln in the local coordinate system by a coordinate transformation according to the stiffness tensor in the total coordinate system(i.e.the coordinate system with one axis pointing vertical downward)as follows(Ting 1996):

c i jln=T im T jk T lp T nq c o mkpq,m,k,p,q=1,2,(4) where we assume the summation convention for repeate

d indices and T im,etc.denot

e the elements o

f the transformation matrix for

the total coordinate system to the local one and c o

mkpq

denote the

components of the stiffness tensor in the total coordinate system.

We implement the irregular-grid PML method by adding a thin,

even-thickness absorbing layer along the smoothed,curved arti?-

cial boundary.Fig.1shows the PML absorbing layer in the prox-

imity of a curved arti?cial boundary and the local numerical mesh

that accounts for the curved boundary.The mesh is composed of

triangles,thus providing the?exibility for the PML absorbing

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Figure2.Illustration of the local coordinate systems.(x1,x2)is a local

coordinate system related to each grid cell,which is determined by making

x1-axis normal to the arti?cial boundary and pass through the centre of the

grid cell(e.g.node13).(y1,y2)is another local coordinate system related

to each node,which is determined by making y1-axis normal to the arti?cial

boundary and pass through the node(e.g.node k).φandθare angles by

which the local coordinate systems can be rotated to the total coordinate

system(z,x),respectively.Point O denotes the centre of curvature of the

local arti?cial boundary,and r the radius of curvature.

to follow an arbitrary geometrical boundary.To derive the irregular-

grid PML method,two local coordinate systems are used,as illus-

trated in Fig.2.One is the local coordinate system related to each

triangular grid cell,such as(x1,x2)in Fig.2that is determined by

making x1-axis normal to the arti?cial boundary and pass through

the centre of the grid cell(i.e.node13).Another is the local coor-

dinate system related to each node,such as(y1,y2)in Fig.2,that

is determined by making y1-axis normal to the arti?cial boundary

and pass through the node(i.e.node k).However,only the local

geometrical coef?cients that are computed in the local coordinate

system related to the grid cell(i.e.in the x1-x2coordinates),rather

than the two local coordinate systems are used in the numerical

implementation.

We de?ne the damping factors at the centres of the grid cells

inside the PML region(i.e.PML absorbing layer),whose values

are given by d0[1?cos(0.5πa/D)].Here,a is the normal distance

from the centre of the grid cell to the PML interface,as shown in

Fig.1,D is the pre-de?ned thickness of the PML absorbing layer

and d0is a positive constant that reads d0=αc p/D with c p denoting

the P-wave velocity of the local medium andα,a parameter that is

selected in the range6.0<α<8.0.

The split velocity components,v⊥

i and v

i

,are de?ned at the nodes

of the triangular grid cells inside the PML region.Here,superscripts ⊥and denote to coincide with the coordinate axes of the local coordinate system related to the node(i.e.y1-and y2-axes).The

split stress components,τ⊥

i j andτ

i j

,are de?ned at the centres of

the grid cells.Here superscripts⊥and mean to coincide with the coordinate axes of the local coordinate system related to the grid cell (i.e.x1-and x2-axes).The velocity and stress?elds are staggered in time,as is common for the?rst-order systems.3I N T E G R A L F O R M U L AT I O N O F T H E

P M L E Q UAT I O N S

3.1Nodes inside the PML region

We obtain the integral formulation of the split?eld PML method using a triangular discretization in accordance with the grid method (Zhang&Liu1999).Node k inside the PML region,as shown in Fig.1,is considered.First,the PML splitting equations with respect to the local coordinate system related to node k,as(y1,y2)in Fig. 2,are used.Integrating both sides of the PML splitting equations, as shown in eq.(1),over the domain enclosed by the dashed-line contour9-10-11-12-13-4-3-9in Fig.1leads to

ρ

?v⊥i

?t d +

ρd v⊥i d =

9?10···3?9

τi1αd s,

ρ

?v i

?t d =

9?10···3?9

τi2βd s,(5)

whereαandβare direction cosines of the outward-directed normals to the contour.Applying the lumped-mass model to eq.(5),that is, lumping the values ofρandρd inside the grid cells to its nodes and setting the values ofρandρd to zero in the inner domain of the grid cell,the surface integrals of the left-hand sides of eq.(5)reduce

to M k(?v⊥

i

/?t)k,Q k(v⊥i)k and M k(?v i/.?t)k.Here,(?v⊥i/.?t)k and

(?v

i

/.?t)k are the?rst-order time derivatives of v⊥i and v i at node

k and(v⊥

i

)k is the value of v⊥

i

at node k.Due to the fact that the dashed-line contour used cuts one-third of the area of each triangular

grid cell,M k and Q k are equal to one-third of the sums of the value

ρd and

ρd d inside each grid cell of the grid cells around node k,respectively.

The discretization of triangular grid cells leads to linear inter-polating functions of the velocity components inside the grid cells. From the point of view of numerical computation,the stresses com-ponents,τi j,become constants within each grid cell.Thus,the right-hand sides of eq.(5)can be rewritten as

9?10···3?9

τi1αd s=

m

n=1

τi1

s n

αd s≈

m

n=1

(τi1)n(b k)n,

9?10···3?9

τi2βd s=

m

n=1

τi2

s n

βd s≈?

m

n=1

(τi2)n(c k)n,

(6) where subscript n denotes the values of the variables in the n th grid cell around node k,m is the number of grid cells around node k and b k and c k are the geometrical coef?cients of the grid cells. Due to the fact that eq.(5)is derived in the local coordinate sys-tem related to node k,as(y1,y2)in Fig.2,b k and c k should be computed in the y1-y2coordinates.For a typical grid cell kpq, with(z p,x p),(z q,x q)and(z k,x k)denoting,respectively,the coor-dinates of nodes p,q and k in the total coordinate system andθdenoting the rotation angle of(y1,y2)to the total coordinate sys-tem(z,x),as illustrated in Fig.2;the exact b k and c k are given by

b k=0.5[(x q?x p)cosθ?(z q?z p)sinθ],

c k=0.5[(z q?z p)cosθ+(x q?x p)sinθ].(7) However,for a smoothe

d arti?cial boundary,w

e haveθ?φ< 0.5 /.r as illustrated in Fig.2.Here,1/.r is the curvature o

f the local arti?cial boundary and is the length of the edge of the grid cell.We can ignore the difference betweenθand

φwhen r>100 (which can be easily satis?ed in building the numerical models).To replaceθwithφin eq.(7),b k and c k become equal to the geometrical

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1032H.Gao and J.Zhang

coef?cients computed in the local coordinate system related to grid

cell kpq ,as (x 1,x 2)in Fig.2.We call the resulting coef?cients the local geometrical coef?cients,which are determined by substituting the coordinates of three nodes of the grid cell in the total coordinate system and the rotation angle of the local coordinate system related to the grid cell against to the total coordinate system (as φin Fig.2)into eq.(7).The other local geometrical coef?cient b p and c p ,etc.,can be obtained by letting k →p →q →k .

We use the local geometrical coef?cients rather than the exact b k and c k in eq.(6).For the same sake (i.e.the difference between the rotation angles can be ignored),we replace the stresses that are de?ned in the local coordinate system related to node k with those de?ned in the local coordinate system related to each grid cell in eq.(6).This is the reason why we use the approximation signs in eq.(6).The proposed approximations lead to a simpler numerical implementation,that is,the same stresses and same local geometrical coef?cients can be used for the integral formulation at the other nodes of the grid cell,such as node p and q .Moreover,the same local geometrical coef?cients can be used to calculate the stresses as discussed in the following.

From eq.(6),we have the integral formulation of the PML split-ting equations using a triangular discretization as follows:M k

?v ⊥i

?t k

+Q k v ⊥i k =m n =1

(τi 1)n (b k )n ,M k ?v

i ?t k

=?m n =1

(τi 2)n (c k )n ,(8)

where the split velocity components are de?ned in the local coor-dinate system related to each node,and the stress components are de?ned in the local coordinate system related to each grid cell.For a typical grid cell pqk ,by constructing the linear interpolating function passing through the nodes of the triangle and then taking ?rst-order spatial derivatives of the function,we have the triangular-grid ?nite-difference operators (e.g.Cook 1974)as

?v l

1≈D 1v l =?1A r =p ,q ,k b r (v l )r ,?v l ?x 2≈D 2v l =1A

r =p ,q ,k

c r (v l )r ,(9)

where A is the area of triangle,subscript r denotes the node of triangle,and coef?cients b r and c r are the same local geometrical coef?cients,as used in eq.(8).Again,we ignore the small difference between the rotation angles of the local coordinate systems related to the grid cell and its nodes.As a result,we can directly substitute the velocity components de?ned in the local coordinate system related to each node,rather than true ones de?ned in the local coordinate system related to the grid cell,into the ?nite-difference operators of eq.(9).We thus have the discretized version of eq.(2)within each grid cell as

?τ⊥i j

n

+(d )n τ⊥i j n

=c i jl 1D 1v l , ?τ i j n

=c i jl 2D 2v l ,(10)where subscript n denotes the value at the centre of the n th grid cell,

the velocities and stresses used are de?ned in the local coordinate systems related to each node and grid cell,respectively.

Eqs (3),(8)and (10)represent the formulations to update the velocities and stresses for the nodes and grid cells inside the PML region.Like the grid method,the approximations in eqs (8)and (10)are second order.Owing to the use of the local geometrical coef?cients,no coordinate transformations arise.

3.2Nodes on the PML interface

When the nodes are on the PML interface (i.e.the arti?cial bound-ary shown in Fig.1),the difference of the coordinate systems has to be considered in deriving the integral formulation of the PML equations.In the following,node g on the PML interface,as shown in Fig.1,is considered.By following the foregoing derivation,inte-grating both sides of the PML splitting equations with respect to the local coordinate system related to node g ,over the domain enclosed by the contour 1-2-3-4-5-g -1in the lower of Fig.1,leads to M g

?v ⊥

i ?t g +Q g v ⊥i g =m 1

n =1(τi 1)n b g n + 5?g ?1τi 1αd s ,M g ?v

i ?t g

=?m 1

n =1

(τi 2)n c g n + 5?g ?1τi 2βd s ,

(11)where M g and Q g are one-third of the sums of the value

ρd and ρd d within each grid cell of the grid cells around node g inside the PML region,respectively.Integrating both sides of eq.(1)with respect to the total coordinate system over the domain enclosed by the contour 5-6-7-8-1-g -5in the upper of Fig.1leads to M

g

?ˉv ⊥

i ?t g =m 2

n =1

(ˉτi 1)n ˉb g n + 1?g ?5ˉτi 1ˉαd s ,M g ?ˉv

i ?t g

=?m 2

n =1

(ˉτi 2)n ˉc

g n + 1?g ?5ˉτi 2ˉβd s ,(12)

where no damping factors are present since they are zero outside the PML region,M

g is one-third of the sum of the value

ρd within each grid cell of the grid cells around node g outside the PML region and the bars above the variables denote that the variables are de?ned in the total coordinate system.

The sums of the two last terms in the right-hand sides of eq.(12)are equal to the total loads acting on interface 1-g -5in the verti-cal and horizontal directions,respectively,F z and F x as shown in Fig.1.The continuities of the stress and velocity components across the PML interface give

?v ⊥

i ?t g =2 k =1

T ik ?ˉv

⊥k ?t

g , ?v i ?t g

=2 k =1T ik ?ˉv

k ?t g

,

5?g ?1

τi 1αd s =?

2 k =1

T ik

1?g ?5

ˉτk 1ˉαd s

,

5?g ?1

τi 2βd s =?

2 k =1

T ik

1?g ?5

ˉτk 2ˉβ

d s

,(13)

where T ik denote the elements of the transformation matrix for

the total coordinate system to the local one.Based on eq.(13),multiplying the transformation matrix to both sides of eq.(12)

and

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then adding them to eq.(11),respectively,lead to

M g +M

g

?v ⊥i

?t g

+Q g v ⊥i g =m 1

n =1(τi 1)n b g n +2 k =1T ik m 2 n =1

(ˉτk 1)n ˉb g

n

,

M g +M

g

?v i

?t g

=?m 1 n =1(τi 2)n c g n ?2 k =1

T ik m 2 n =1

(ˉτk 2)n ˉc

g

n .(14)

Eq.(14)represents the integral formulation of the PML splitting

equations,using triangular grid discretization for the nodes on the PML interface.Following the discussions on M g and M g below eqs

(11)and (12),we know M g +M g and Q g are one-third of the sums of the value ρd and

ρd d within each grid cell of all the grid cells around node g (no matter whether inside and outside the PML region),respectively.Hence,the left-hand sides of the resulting integral formulation are same for the nodes on the PML interface and inside the PML region.The only difference between the integral formulations is that a coordinate transformation is needed for the grid cells outside the PML region.

Eqs (3)and (14)represent the formulations to update the veloc-ities of the nodes on the PML interface.For the nodes outside the PML region,the integral formulation of eq.(1)are the same as ones used in the grid method,which are the sum of the two equations in eq.(8)with Q k related terms and split velocity ?eld vanishing.The numerical implementation becomes simple when incorporating the irregular-grid PML model into the grid method owing to the similar integral formulation for the nodes inside the PML region,on the PML interface and outside the PML region.

4N U M E R I C A L I M P L E M E N TAT I O N S The numerical implementation of the grid method is completed by looping through each grid cell and adding the results obtained to the memory units corresponding to the nodes (Zhang &Liu 1999).Based on the pre-calculated local geometrical coef?cients and elastic stiffness tensors (which are needed only in anisotropic cases),we can update the split stresses and velocities of the nodes and grid cells inside the PML region,following the same numerical procedure as the grid method,by looping through each grid cell inside the PML region.Hence,we can combine the updates of the stresses and velocities inside and outside the PML region by looping through all grid cells together,when incorporating the irregular-grid PML model into the grid method.

There are two differences between the updates inside and outside the PML region.In particular:(1)two results of the right-hand sides of eq.(8)are summed and then added to one memory unit for the grid cells outside the PML region,whereas the two results are added to the separated memory units for the grid cells inside the PML region and (2)the geometrical coef?cients b k and c k are picked up from the different tables,and the split stress ?elds are computed for the grid cells inside the PML region.Special treatments are needed for the grid cells that have nodes on the PML interface but are outside the PML region.That is,the results obtained using those grid cells should ?rst be subjected to coordinate transformation and then added to the corresponding memory units,as expressed in eq.(14),when the related nodes are on the PML interface.

We can update the split velocity ?elds at the nodes on the PML

interface and inside the PML region based on the results of the right-hand sides of eqs (8)and (14)(which have been obtained by looping through all grid cells)using the centre-difference approximations that read

?v ⊥i

?t t +0.5 t

k =1 t v ⊥i t + t k ? v ⊥i t k ,

v ⊥i t +0.5 t k =12

v ⊥i t + t k + v ⊥i t k ,(15)

where the superscript denotes the time.The split stress ?elds inside the PML region can be updated,based on the results of the right-hand sides of eq.(10)(which are obtained using the triangular-grid ?nite-difference operators of eq.9),by using the same centre difference approximations as eq.(15).We update the velocity and stress ?elds outside the PML region using the same but simpler procedure,as discussed in Zhang &Liu (1999),because the damping terms vanish and no split ?elds are needed.We can thus update the velocities from time level t to t + t and stresses from time level t ?0.5 t to t +0.5 t in the whole domain.

The local geometrical coef?cients and the elastic stiffness tensor (which are needed only in anisotropic cases)are computed and stored in a table in advance.We can then pick up them from the table for the recursive computations.Hence,no extra computational costs arise when the irregular-grid PML method is used,as well as when the anisotropy is considered.The same numerical procedure,for the grid cells inside and outside the PML region,leads to a simple computer implementation when incorporating the irregular-grid PML model into the grid method.

The resulting irregular-grid PML model can also be in other numerical schemes which employ the ?rst-order system.For this sake,the mesh composed of triangles should be generated inside the PML absorbing layer and in its neighbourhood.The updates of the splitting stresses and velocities at the nodes inside the PML region and on the PML interface can be completed by looping through those triangular grid cells,as discussed earlier.The stresses and velocities at nodes that are not enclosed by the triangular grid cells need to be updated using the corresponding numerical schemes.Hence,the irregular-grid PML model can also be used to construct ?exible arti?cial boundaries by the other numerical schemes.5N U M E R I C A L E X A M P L E S 5.1Wave propagation in a VTI half-space

This example considers the anisotropic Lamb’s problem.We use the grid method together with the irregular-grid PML model.A semi-circle is taken as an arti?cial boundary and an even-thickness PML absorbing layer is imposed along the boundary.The numerical mesh is composed of homogeneous right triangles with the right edge of 5m inside and outside the PML region.Due to anisotropy and the lower surface wave velocity,we use a little thicker PML absorbing layer that has 15grid cells in thickness with d 0=224.0s ?1.The medium is a transversely isotropic medium with a symmetry axis normal to the surface.Its ?ve modi?ed Lam′e parameters and density are listed in Table 1,where subscript means the variable parallel

Table 1.Elastic constants of the VTI and TTI media.

Medium λ (GPa)μ (GPa)λ⊥(GPa)μ⊥(GPa)η(GPa)ρ(kg m ?3)VTI 6.99 5.32 3.288.99 5.632340TTI

6.71

9.38

7.29

5.55

10.44

2440

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X-axis (m)Figure 3.Snapshots of the norm of the velocity for a VTI lamb’s problem with and without absorbing boundaries at 0.317and 0.505s propagation times.Owing to the symmetry,only the half for each case is shown.The left-hand sides are the results obtained using a rectangular non-absorbing boundary,and the right-hand sides are the results obtained using a semi-circle PML absorbing layer,represented by two parallel solid lines.Note the events that are gradually decaying inside the PML absorbing layer.

to the symmetry axis.The VTI medium has a quasi-P wave velocity of 2745m s ?1and a quasi-SV wave velocity of 1508m s ?1in the vertical direction.A Ricker-wavelet vertical force is loaded at the surface with a peak frequency of 20Hz.For contrast,we also compute the case where a rectangular non-absorbing boundary is used.Both results are symmetric.For comparison,we incorporate each half of the two results into a ?gure,as shown in Fig.3.

Fig.3shows snapshots of the norm of the velocity, v =

v 21+v 22,at 0.317and 0.505s propagation times for the two cases.By comparing the right-and left-hand sides,we see that the conical and quasi-P waves that propagate through the PML absorbing layer at 0.317s are gradually decaying,whereas all the surface wave,conical wave and quasi-P and quasi-SV waves are well absorbed by the PML layer,without re?ections,at 0.505s.In this example,a staircase approximation is used to model the semi-circle arti?cial boundary in the numerical discretization.This shows that it is not necessary to accurately follow the prescribed arti?cial boundary in generating the mesh inside the PML https://www.doczj.com/doc/821273484.html,pared with the rect-angular boundary,the curved arti?cial boundary used results in a 21per cent reduction in the computational cost and storage require-ments.We also avoid the complexity resulting from the corners,which will occur in the conventional PML model.

5.2Wave propagation in a homogeneous TTI medium We use the grid method,together with the irregular-grid PML model,

to simulate quasi-P and quasi-SV wave propagation in a homoge-neous TTI medium.The TTI medium is a transversely isotropic medium with a symmetry axis of 30?to the vertical direction.Its ?ve modi?ed Lam′e parameters and density are listed in Table 1,

where subscript means the variable parallel to the symmetry axis.The medium has a quasi-P wave velocity of 3231m s ?1and a quasi-SV wave velocity of 1961m s ?1,in the direction parallel to the symmetry axis.We use an elliptical arti?cial boundary.A PML absorbing layer with a thickness of 15grid cells and d 0=549.0s ?1is imposed along the curved arti?cial boundary.The numerical mesh is composed of homogeneous right triangles with the right edge of 3m inside and outside the PML region.A Ricker-wavelet point source,with a peak frequency of 20Hz,is positioned above of the centre,as indicated by cross in Fig.4.As a result,waves will arrive at the upper and lower arti?cial boundaries at the different propagation times.

Fig.4shows snapshot of the norm of the velocity, v =

v 21+v 22,at 0.325and 0.625s propagation times.We see that quasi-P wave is absorbed and quasi-SV wave is partially absorbed in the upper of the ?gure at 0.325s.Quasi-P wave is fully absorbed,and only a part of quasi-SV wave that doesn’t arrive at the PML absorbing layer can be seen,at 0.625s.

5.3Wave propagation in an isotropic medium with curved surface and interface

We use the grid method together with the irregular-grid PML model to simulate elastic wave propagation in a two-layer isotropic medium with curved interface and surface,as shown in Fig.5.The ?rst and second layer media have P -wave velocities of 3231and 3749m s ?1,S -wave velocities of 1960and 2621m s ?1and densities of 2440and 2920kg m ?3,

respectively.A numerical discretization of inho-mogeneous triangular grid cells is used that accurately model the surface and interface topographies.The edge of the triangular grid

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0500

10001500

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X-axis (m)t=0.325 s t=0.625 s

PML Layer

PML Layer

Figure 4.Snapshots of the norm of the velocity for a point source in a TTI

medium at 0.325and 0.625s propagation times.Cross indicates the point source.An elliptical PML absorbing layer,represented by two parallel solid lines,is used to simulate the unbounded medium.Note the events that are gradually decaying inside the PML absorbing layer.Quasi-P wave is fully absorbed and only a part of quasi-SV wave can be seen in the lower ?gure.

cell is varying around 3m.A semi-ellipse PML absorbing layer,as shown in Fig.5,is imposed along the curved arti?cial boundary.The thickness of the PML layer is 10grid cells with d 0=692.0s ?1in the ?rst-layer and d 0=803.0s ?1in the second-layer.Again,we use a staircase approximation to simulate the curved arti?cial boundary in the numerical discretization.

A Ricker-wavelet pressure source with a peak frequency of 40Hz is positioned 130m below the surface,as indicated by cross in Fig.5.Fig.5shows snapshots of the vertical component of the velocity at 0.202and 0.307s propagation times.By contrast,Fig.6shows the same snapshots at the same times for the same model as Fig.5,when a rectangular non-absorbing boundary is used.The re?ections and refractions from the curved surface and interface are well modelled owing to the accurate descriptions of the topographies in the numerical discretization.By comparing Figs 5and 6,we see that the direct and transmitted P -waves,as well as converted

S -wave,that arrive at the PML absorbing layer are well absorbed at 0.202s.The re?ected and transmitted S -waves and sur-face and interface waves that arrive at the PML absorbing layer are absorbed without re?ections at 0.307s

in Fig.5,yet a lot of re?ected

Z -a x i s (m )

X-axis (m)

Z -a x i s (m )

Figure 5.Snapshots of the vertical component of the velocity for a two-layer,isotropic,elastic model at 0.202and 0.307s propagation times.The curved surface and interface are represented by solid lines.A semi-elliptical PML absorbing layer,represented by two parallel solid lines,is used to simulate the half-in?nite medium.Cross indicates the pressure source.The re?ections and refractions from the curved surface and interface are well modelled.No re?ections resulting from the arti?cial boundary can be seen.

waves,resulting from the arti?cial boundaries,are seen in the snap-shots of https://www.doczj.com/doc/821273484.html,pared with the rectangular arti?cial boundary

used in Fig.6,the semi-ellipse arti?cial boundary used in Fig.5results in a 22per cent reduction of the discretized nodes.This means a 22per cent reduction in computational cost and storage requirements.

6C O N C L U S I O N S

We have implemented the PML absorbing boundary condition on an arbitrary geometrical boundary,using a triangular discretization,which results in an irregular-grid PML method that has the abil-ity to absorb incident waves in arbitrary directions.The irregular-grid PML method is developed,following the grid method,which can absorb both body and surface waves in elastic isotropic and anisotropic media.The irregular-grid PML method can also be in other numerical schemes that employ the

?rst-order formulation to simulate unbounded media.The method enables the use of fewer nodes since arti?cial absorbing boundaries can be implemented along smooth curved interfaces.The irregular-grid PML method is simple to implement in conjunction with the grid method,and no extra computational effort is introduced for anisotropic media

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500

750

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500

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250

500

750

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0250

500750

1000

X-axis (m)t=0.202 s

Surface

t=0.307 s

Surface

Figure 6.The same snapshots as Fig.5when a rectangular non-absorbing boundary is used.The white-line semi-ellipse denotes the PML interface used in Fig.5.

compared with isotropic media.No additional computational cost is required for using the irregular-grid PML method,in contrast to standard PML implementations,and no special treatment of corners is necessary.Numerical experiments demonstrate its desired effects and a signi?cant reduction of the discretized nodes.A C K N O W L E D G M E N T S

Thanks to the National Natural Science Fund of China (under grant 40474046),which supported this work.This work was also sup-ported by the National High-tech R&D Program of China (under

grant 2006AA09A102)and National Basic Research Program of

China (under grant 2005CB422104).

R E F E R E N C E S

B′e renger,J.,1994.A perfectly matched layer for the absorption of electro-magnetic waves,https://www.doczj.com/doc/821273484.html,put.Phys.,114,185–200.

Collino,F .&Tsogka,C.,2001.Application of the perfectly matched ab-sorbing layer model to the linear elastodynamic problem in anisotropic heterogeneous media,Geophysics,66,294–307.

Cook,R.D.,1974.Concepts and Applications of Finite Element Analysis,John Wiley &Sons Inc.,New Y ork.

Festa,G.&Vilotte,J.-P .,2005.The newmark scheme as velocity-stress time-staggering:an ef?cient PML implementation for spectral element simulation of elastodynamics,Geophys.J.Int.,161,789–812.

Gao,H.&Zhang,J.,2006.Parallel 3-D simulation of seismic wave prop-agation in heterogeneous anisotropic media:a grid method approach,Geophys.J.Int.,165,875–888.

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Marcinkovich,C.&Olsen,K.,2003.On the implementation of perfectly matched layers in a three-dimensional fourth-order velocity-stress ?nite difference scheme.J.geophys.Res.,108(B5),2276.

Moczo,P .,1989.Finite-difference technique for SH-waves in 2-D media using irregular grid:application to seismic response problem.Geophys.J.Int.,99,321–329.

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Wang,T.&Tang,X.,2003.Finite-difference modeling of elastic wave propagation:a nonsplitting perfectly matched layer approach.Geophysics,68,1749–1755.

Zhang J.,1997.Quadrangle grid velocity stress ?nite difference method for elastic wave propagation simulation,Geophys.J.Int.,131,127–134.

Zhang,J.,2001.Triangle-quadrangle grid method for poroelastic,elastic,and acoustic wave equations,https://www.doczj.com/doc/821273484.html,p.Acoust.,9,681–702.

Zhang,J.,2004a.Elastic wave modelling in heterogeneous media with high velocity contrasts,Geophys.J.Int.,159,223–239.

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Zhang,J.,2005.Elastic wave modeling in fractured media with an explicit approach,Geophysics,70,T75–T85.

Zhang,J.&Liu,T.,1999.P-SV -wave propagation in heterogeneous media:grid method,Geophys.J.Int.,136,

431–438.

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如何写先进个人事迹

如何写先进个人事迹 篇一:如何写先进事迹材料 如何写先进事迹材料 一般有两种情况:一是先进个人,如先进工作者、优秀党员、劳动模范等;一是先进集体或先进单位,如先进党支部、先进车间或科室,抗洪抢险先进集体等。无论是先进个人还是先进集体,他们的先进事迹,内容各不相同,因此要整理材料,不可能固定一个模式。一般来说,可大体从以下方面进行整理。 (1)要拟定恰当的标题。先进事迹材料的标题,有两部分内容必不可少,一是要写明先进个人姓名和先进集体的名称,使人一眼便看出是哪个人或哪个集体、哪个单位的先进事迹。二是要概括标明先进事迹的主要内容或材料的用途。例如《王鬃同志端正党风的先进事迹》、《关于评选张鬃同志为全国新长征突击手的材料》、《关于评选鬃处党支部为省直机关先进党支部的材料》等。 (2)正文。正文的开头,要写明先进个人的简要情况,包括:姓名、性别、年龄、工作单位、职务、是否党团员等。此外,还要写明有关单位准备授予他(她)什么荣誉称号,或给予哪种形式的奖励。对先进集体、先进单位,要根据其先进事迹的主要内容,寥寥数语即应写明,不须用更多的文字。 然后,要写先进人物或先进集体的主要事迹。这部分内容是全篇材料

的主体,要下功夫写好,关键是要写得既具体,又不繁琐;既概括,又不抽象;既生动形象,又很实在。总之,就是要写得很有说服力,让人一看便可得出够得上先进的结论。比如,写一位端正党风先进人物的事迹材料,就应当着重写这位同志在发扬党的优良传统和作风方面都有哪些突出的先进事迹,在同不正之风作斗争中有哪些突出的表现。又如,写一位搞改革的先进人物的事迹材料,就应当着力写这位同志是从哪些方面进行改革的,已经取得了哪些突出的成果,特别是改革前后的.经济效益或社会效益都有了哪些明显的变化。在写这些先进事迹时,无论是先进个人还是先进集体的,都应选取那些具有代表性的具体事实来说明。必要时还可运用一些数字,以增强先进事迹材料的说服力。 为了使先进事迹的内容眉目清晰、更加条理化,在文字表述上还可分成若干自然段来写,特别是对那些涉及较多方面的先进事迹材料,采取这种写法尤为必要。如果将各方面内容材料都混在一起,是不易写明的。在分段写时,最好在每段之前根据内容标出小标题,或以明确的观点加以概括,使标题或观点与内容浑然一体。 最后,是先进事迹材料的署名。一般说,整理先进个人和先进集体的材料,都是以本级组织或上级组织的名义;是代表组织意见的。因此,材料整理完后,应经有关领导同志审定,以相应一级组织正式署名上报。这类材料不宜以个人名义署名。 写作典型经验材料-般包括以下几部分: (1)标题。有多种写法,通常是把典型经验高度集中地概括出来,一

关于时间管理的英语作文 manage time

How to manage time Time treats everyone fairly that we all have 24 hours per day. Some of us are capable to make good use of time while some find it hard to do so. Knowing how to manage them is essential in our life. Take myself as an example. When I was still a senior high student, I was fully occupied with my studies. Therefore, I hardly had spare time to have fun or develop my hobbies. But things were changed after I entered university. I got more free time than ever before. But ironically, I found it difficult to adjust this kind of brand-new school life and there was no such thing called time management on my mind. It was not until the second year that I realized I had wasted my whole year doing nothing. I could have taken up a Spanish course. I could have read ten books about the stories of successful people. I could have applied for a part-time job to earn some working experiences. B ut I didn’t spend my time on any of them. I felt guilty whenever I looked back to the moments that I just sat around doing nothing. It’s said that better late than never. At least I had the consciousness that I should stop wasting my time. Making up my mind is the first step for me to learn to manage my time. Next, I wrote a timetable, setting some targets that I had to finish each day. For instance, on Monday, I must read two pieces of news and review all the lessons that I have learnt on that day. By the way, the daily plan that I made was flexible. If there’s something unexpected that I had to finish first, I would reduce the time for resting or delay my target to the next day. Also, I would try to achieve those targets ahead of time that I planed so that I could reserve some more time to relax or do something out of my plan. At the beginning, it’s kind of difficult to s tick to the plan. But as time went by, having a plan for time in advance became a part of my life. At the same time, I gradually became a well-organized person. Now I’ve grasped the time management skill and I’m able to use my time efficiently.

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