V.C.Loukopoulosand G.C.Bourantas
The meshless(or meshfree)methods are being actively developed as a powerful numerical tool for various engineering and physical applications.The primary reason for the significant interest in meshless computational procedures is that most of the established numerical techniques,such as the Finite Element Method(FEM),the Finite Volume Method(FVM),the Finite Difference Method(FDM)and the Spectral Method(SP)require a mesh.The automatic generation of a good quality mesh poses a significant problem in the analysis of practical engineering systems.Moreover,the simulation and the analysis of certain types of problems(like dynamic crack propagation,pulsatile and transient flows)often require an expensive remeshing operation.Meshless techniques overcome these difficulties,associated with the meshing and re-meshing procedures,by eliminating the mesh altogether.Interpolation is performed in terms of nodal points scattered at the spatial domain using functions having compact support.A weighted residual technique is used to generate the discrete set of equations corresponding to the governing partial differential equations[Liu(2003),Liu and Gu(2005)].
Since the meshless methods emerged as a potential alternative for solutions in computational mechanics,a variety of such approaches have appeared.Over the last decades,several meshfree methods have been proposed since the prototype of the meshfree methods,the Smoothed Particle Hydrodynamics(SPH),was born[Gingold and Monaghan(1977)].These methods include the Diffuse Approximation Method(DAM)[Nayroles,Touzot and Villon(1991)],that is closely related to the Moving Least Squares method;the Diffuse Element Method(DEM)[Nayroles,Touzot and Villon(1992)],developed by the Moving Least Squares approximation,and the Element Free Galerkin method(EFG)[Lu,Belytschko and Gu(1994)];the Reproducing Kernel Particle Method(RKPM)[Liu,Jun and Zhang(1995),Liu,Jun,Li,Adee and Belytschko(1995)],which is used to improve the SPH approximation;the Partition of Unity Finite Element Method(PUFEM)[Melenk and Babuska(1996)];thehp-Clouds[Duarte and Oden(1996)];the Moving Least-Square Reproducing Kernel Method(MLSRK)[Liu,Li and Belytschko(1996)];the meshless Local Boundary Integral Equation Method(LBIE)[Zhu,Zhang and Atluri(1998)];the Meshless Local Petrov–Galerkin method(MLPG)[Atluri,Kim and Cho(1999),Atluri and Shen(2002)];the Finite Point method(FPM)[Onate,Idelsohn,Zienkiewicz and Taylor(1995)];the meshless point collocation methods(MPC)[Aluru(2000)],and more.
The present paper is referred to the numerical computation of the two-dimensional(2D)time-dependent Schr?dinger equation.Linear Schr?dinger equation is written as
in some continuous domain with suitable initial Dirichlet and Neumann boundary conditions and an arbitrary potential functionV(x,y).The corresponding initial condition is given by
and the boundary conditions by
wherei=is the unit imaginary number,Tis the final time,h,sandgare known functions,and??=??D∪??N,where??Dand??Nare the Dirichlet and the Neumann parts of the boundary?? andnnnis the unit outward vector to??.This type of partial equation models many physical problems and find applications in quantum mechanics and various quantum dynamics calculations[Arnold(1998),Hajj(1985),Ixaru(1997)],in electromagnetic wave propagation and the design of certain optoelectronic devices[Levy,(2000),Huang,Xu,Chu and Chaudhuri(1992)],and finally,in underwater acoustics[Tappert(1977)].The time-dependent Schr?dinger equation can be represented in a hydrodynamical form,called a quantum hydrodynamic(QHD)equation,a formulation which is analogous to the equations of irrotational motion in a classical fluid[Gasser,Lin and Markowich(2000),Kalita,Chhabra and Kumar(2006)].In this formulation,system(1)is replaced by a system of partial differential equations in terms of particle density and velocity potential,by separating the real and imaginary parts of a general solution
obtained by expressing ψ as ψ=u+iυ,whereuand υ are real-values functions.There have been numerous attempts to develop numerical schemes for equations(1)or the system(2).In[Simos(2008),Simos(2007)]trigonometrically- fitted methods were utilized for the numerical solution of the Schr?dinger equation.The authors of[Kalita,Chhabra and Kumar(2006),Subasi(2002)]studied models similar to the present problem using finite-difference techniques.Finite-difference methods are well-known as the first technique for solving partial differential equations(PDEs).In[Dehghan(2002)]explicit finite difference methods were used for solving the governing equations,while in[Dehghan(1999)]the need of using a large amount of CPU time in implicit finite-difference schemes limit the applicability of these methods.Furthermore,these methods provide the solution of the problem on mesh points only,and the accuracy of the techniques is reduced in non-smooth and non-regular domains.Thus,alternative computational methods,such as global Radial Basis Functions[Dehghan and Shokri(2007)],were used for the numerical solution of the Eq.(1).In the present paper we investigate a different approach to find the solution of linear and nonlinear Schr?dinger equation.We present a numerical scheme to solve the two-dimensional(2D)time-dependent Schr?dinger equation using the Collocation method,while we approximate the solution directly using Moving Least Squares.Actually,the meshless point collocation(MPC)method is a case of MLPG when the collocation Dirac’s Delta function is used as the test function[Atluri and Shen(2002)].To test the robustness,the accuracy and the efficiency of the proposed scheme,it is applied to four examples having analytical solutions,with our results exhibiting very good agreement with the analytical ones.Additionally,our results are compared with a meshless collocation and radial basis function method using multiquadrics(MQ)and the Thin Plate Splines(TPS).The layout of the paper is as follows.In Section 2 we present the methodology for the implementation of the Moving Least Squares approximation for the solution of QHD equations.In Section 3 we apply this technique on the two-dimensional(2D)time-dependent Schr?dinger equation.The results of the numerical experiments are presented in Section 4,while Section 5 is dedicated to a brief conclusion.
In the moving least-squares technique,the approximationuh(xxx)is expressed as the inner product of a vector of the polynomial basis,ppp(xxx)and a vector of the coefficients,aaa(xxx)
whereppp(xxx)∈RRRm,aaa(xxx)∈RRRmandmis the number of monomials in the polynomial basis(in the present studym=6).The local character of the moving least-squares(MLS)approximation can be viewed as a generalization of the traditional leasts-quares approximation,in which the vectoraaais not a function ofxxx.
Equation(3)is commonly referred to as the global least-squares approximation.In addition,there exists a unique local approximation associated with each point in the domain.In order to determine the form ofaaa(xxx),a weighted discrete error norm,
is constructed and sequentially minimized.Here,wI(xxx)denotes the weight function,wI(xxx)≡w(xxx?xxxI),associated with nodeI,and the quantity in brackets is the difference between the local approximation at nodeIand the data at nodesI,that isui,andnis the number of nodes in the support ofwI(xxx).The minimization of Eq.(4)with respect toaaa(xxx)determinesaaa(xxx).The local approximation associated with pointxxxis used only in the minimization process and is equivalent to the global approximation at the single pointxxx.Compact support of the weight functions gives the moving least-squares method its local character.
The minimization of Eq.(4),
results in the linear system
whereUUUsis a vector containing the nodal data,=[u1,u2,...,un],and
whereAAA∈RRRm×mandBBB∈RRRm×n.The matrixAAAmust be inverted at every sampling point.Substitution of the solution of(Eq.(6))into the global approximation(Eq.(3)),completes the least-squares approximation,
Here,the spatial dependence has been lumped into one row matrix, ?(xxx)and,therefore,the approximation takes the form of a product of a matrix of shape functions with a vector of nodal data.Derivatives of the shape functions may be calculated by applying the product rule to
In order to obtain the spatial derivatives of the approximation function,uh(xx x),it is necessary to obtain the derivatives of the MLS shape functions,?i(xx x),
The derivative of the shape function is given as
wherexj=x,y,zand
The weight function is non-zero over a small neighborhood ofxxxi,called the support domain of nodei.The choice of the weight functionW(xxx?xxxi)affects the resulting approximationuh(xxxi)inherently.In the present paper a Gaussian weight function is used[Liu(2003),Bourantas,Skouras and Nikiforidis(2009)],yet the support domain does not have a standard point density value.Instead,a constant number of nodes are used for the approximation of the field function.
whereI=1,2,3,...,qare the nodes that produce the support domain of nodexi,andwitha0a prescribed constant(oftena0=0.2).
The Meshless Point Collocation method is a MFree“strong-form”description method.The“strong-form”of the governing equations and the boundary conditions are used and discretized by collocation techniques.The aforementioned formulations possess the following attractive advantages.They are truly meshless and the implementing procedure is straightforward,while the algorithms and the implementation can be kept simple,particularly when handling problems with Dirichlet boundary conditions solely.Under these conditions,these methods are highly efficient computationally,even with the application of polynomial approximation functions,and the solution can be systematically obtained with increased accuracy,compared to FEM,FVM,FDM,or other computational methods.In general,MFree strong-form methods may still suffer from some local stability and accuracy issues,depending on the problem[Liu and Gu(2005)].However,these local restrictions are now systematically avoided with the utilization of specific nodal distributions(Type-I)and proper local point cloud refinement procedures,in accordance with[Bourantas,Skouras and Nikiforidis(2009),Kim and Liu(2006)],even for natural or mixed type boundary conditions.The robustness of these methods has,however,been an issue especially for scattered set of points.The stability and the convergence of the collocation methods are ensured by the resulting linear or linearized algebraic system.If the latter possesses some attractive features then both the stability and the convergence are ensured.In fact,the robustness of the collocation methods can be improved by understanding the possible sources of errors.specifically,the errors could arise because of the way the meshless approximation functions and their derivatives have been constructed for a scattered set of points or because of the way the discretization of the governing equations has been performed.When the meshless approximation functions and its derivatives do not satisfy certain conditions(referred to as the positivity conditions)for a given point distribution,it is possible to get large numerical errors when using collocation methods.To satisfy the positivity conditions,the weighting function used in the construction of the approximation functions can play an important role.These studies suggest that positivity conditions can be important when using meshless collocation methods.Additionally,the convergence of the discrete Laplacian operator for Dirichlet boundary conditions has been proved when a regular grid(named Type-I)is used.Thus,both the stability and the convergence of the meshless point collocation method,using MLS approximation and regular nodal distribution are ensured.
Collocation method using MLS may be considered as a special case of the“weak–form”methods[Atluri,(2004)].Moreover,this collocation method may be considered as a“weak-solution”,with a Dirac delta function as the test(weight)function[Atluri,Liu and Han(2006)].The weighted residual method provides a flexible mathematical framework for the construction of a variety of numerical solution schemes for the differential equations arising in the field of both science and engineering.Its application,in conjunction with the Moving Least Square(MLS)approximation method, yields powerful solution algorithms for the governing equations.
The collocation scheme using the Moving Least Squares approximation used in the present work and applied for the spatial discretization of the unsteady homogeneous diffusion equation will be discussed next,along with the explicit Euler,θ-weighted time-stepping scheme used for temporal discretization.
Consider the governing equations of the unsteady problem
with the aforementioned boundary and initial conditions.By the MLS approximation one getsfor the unknown function,uq(xxx)=for the partialx,yderivative andthe secondx,ypartial derivative.Additionally,we setndas the number of nodes in the interior,nbas the number of nodes on the boundary,and the final number of nodes asN(N=nd+nb).The first equation,Eq.(15)can be written as
From the notation described above and using the Euler’s θ-weighted time-stepping scheme for temporal discretization,for the interior nodes one gets
Multiplying both parts by δtone gets
In matrix notation, for all points, incorporating the boundary conditions atnbboundary nodes one has
whereGVis the operator defining the boundary conditions for velocity(Dirichlet type on??).
These equations can be written in a more compact manner by setting
Regarding the second Eq.(16)and following the same procedure described for Eq.(15)one can derive(in matrix notation)
whereGBis the operator defining the boundary conditions for the induced magnetic field on??.Once again,the above equations can be written in more compact form by setting
The final system of the QHD coupled partial differential equations can be written as
Finally,setting
the discretized PDEs of QHD fl ow are summed as
In order to examine the validity and the effectiveness of the proposed scheme,four representative case studies were examined[Dehghan and Shokri(2007),Dehghan,and Mirzaei(2008),Dehghan,and Mirzaei(2008)];thee cases for the linear Schr?dinger equation with and without the potential function present,and a fourth one for nonlinear Schr?dinger equation.
Example 1
Initially,we consider the case with potentialV=0 at the Schr?dinger equation,in the spatial domain(0,1)×(0,1)and initial conditions[Dehghan,and Mirzaei(2008)]
which generates the exact solution
The Dirichlet boundary conditions were extracted from the analytical solution.Table 1 presents the relative error of both real and imaginary parts,defined asfort=5 andt=20 sec.The meshless point method with MLS approximation depends on several parameters that have to be chosen properly in order to achieve convergence and accuracy.These parameters include the proper
nodal distribution,the number of nodes in the support domain,and the user-defined variables used in the weight function.For our investigation purposes we use a regular nodal distribution of Type-I[Kim and Liu(2006)],which ensures the fulfillment of the so-called positivity conditions[Jin,Li and Aluru(2004)].Additionally,we set the user-defined parameter α0at the weight function to be α0=0.2,the number of nodes in the support domain 10,and time stepdt=0.05.As pointed out elsewhere[Bourantas,Skouras and Nikiforidis(2009)],when the number of nodes in the total domain is increased,the accuracy is improved.This also is depicted at the Table 1.
The MLS approximation is obtained by a special least-squares method[Liu and Gu(2005)].The function obtained by the MLS approximation is a smooth curve(or surface),which does not pass through the nodal values inherently.Therefore,the MLS shape functions do not,in general,satisfy the Kronecker delta condition.Thus,when the nodes in the support domain increase,the Gaussian weight function loses its local character(delta function property),resulting in truncated errors which decrease the accuracy of the numerical results.Thus,in Table 2,we present the dependence of the accuracy from the number of nodes in the support domain.To do that,we used a constant grid of 31×31 nodes and altered the number of nodes at the support domain.The results obtained show the very good accuracy of the proposed scheme when the number of the nodes in the support domain is kept small.Moreover,in Fig.1,plots are presented for numerical and exact solutions for the real and imaginary part att=20,using a 21×21 regular grid and 10 nodes in the support domain.
Table 1:Relative errors att=5 andt=20 for different grids,dt=0.05 for support domain 10.
Example 2
As a second example,we consider the Schr?dinger equation in the spatial domain(0,1)×(0,1),with potential function[Dehghan and Shokri(2007),Dehghan,and
Table 2:Relative errors at t=5 and t=20 for different number of nodes in the support domain,dt=0.05.
Figure 1:Plots of numerical and exact solutions for the real and imaginary part at t=20,using a 21×21 regular grid and 10 nodes in the support domain.
Mirzaei(2008)]
V(x,y)=3?2tanh2x?2tanh2y.
Initial and boundary conditions are defined as
and
The analytical solution is given by
Table 3 presents the maximum absolute error for the real and the imaginary parts of the solution at different times up tot=1,using meshless point collocation method with MLS approximation.For comparison purposes,numerical results are also presented using meshless collocation method with global Radial Basis Functions approximation using multiquadrics(MQ)and thin plate splines(TPS)respectively[Dehghan and Shokri(2007)].These results were obtained fordx=dy=0.1,anddt=0.001.The maximum relative error,ε,defined as ε=Max(x,y)∈??was also reported.The total number of nodes was 121(11×11),the number of nodes in the support domain was set to 10,ensuring the inversion of the moment matrix,AAA(xxx),and the parameter α0was set to α0=0.2[Liu(2003)].
At Table 4 the CPU time(in seconds)is presented,in order to demonstrate the efficiency of the meshless point collocation method.The shape functions are not pre-defined,and they must be constructed before the numerical solution of the resulting algebraic system.Thus,in our in-house code,the numerical procedure contains two parts; first comes the construction of the shape functions and,then,the solution of the resulting linear system.
Figure 2:Plots of numerical and exact solutions for the real and imaginary part at t=1,using a 11×11 grid.
In Fig.2 the graphs of the real part and the imaginary parts of the numerical and the analytical solutions using MLS are shown at timet=1,withdx=dy=0.1,
dt=0.001.Note that there is no essential divergence between the exact solution and the numerical solution in Fig.2,for the given accuracy.
Table 3:Maximum absolute error of multiquadrics and thin plate spline based scheme at different times with dx=dy=0.1,dt=0.001 and c=0.7 for MQ.For every value of t,the first and second rows of data correspond to the use of MQ,TPS as the radial basis function respectively and the third for the MPC.
Table 4:CPU time in seconds for shape construction and solution of the resulting transient,linear system.
One can notice that,for coarse grids,as in the case of 121 nodes,the numerical results obtained by the meshless point collocation with MLS approximation are less accurate than those obtained by the global multiquadrics Radial Basis Function.Although full-domain RBF methods are highly flexible and can exhibit high-order convergence rates[Madych and Nelson(1990)],in their basic implementation the fully-populated matrix systems produced lead to poor numerical conditioning as the size of the dataset increases.This problem is described by Schaback[Schaback(1993)]as the“uncertainty relation”,in which better conditioning is associated with worse accuracy,and worse conditioning is associated with improved accuracy.With increasingly large datasets and increasingly fl at basis functions,this problem becomes more pronounced.Thus,global RBF are not appropriate for real world applications,were the number of the degrees of freedom(nodes)are large.On the other hand,MLS approximation,being a localized-type approximation,uses a small number of neighboring nodes for interpolation.This makes the MLS approximation more suitable for many applications arising in science and engineering.Furthermore,the small number of nodes used makes the method computationally time and memory saving.This is evident at Table 5 where doubling the nodal distribution density increases the accuracy of the numerical solution by an order of magnitude,while the computational efficiency of the scheme is retained.
Table 5:Absolute and relative errors at different times for dx=dy=0.05 and 0.025,and dt=0.001.
Example 3
Following,we consider the Schr?dinger equation in(0,1)×(0,1)spatial domain and with potential function[Dehghan and Shokri(2007),Dehghan,and Mirzaei(2008)]
and initial and boundary conditions
ψ(x,y,0)=x2y2
and
ψ(0,y,t)=0,ψ(1,y,t)=y2eit,ψ(x,0,t)=0,ψ(x,1,t)=x2eit,
The analytical solution is given as
ψ(x,y,t)=x2y2eit.
Table 6 presents the maximum absolute error for the real part and imaginary part at different times up tot=1,using MLS approximation and time stepdt=0.05.The results obtained were compared with those obtained using the multiquadrics and the thin plate spline RBF with the same nodal distribution and time step,dt=0.0005[Dehghan and Shokri(2007)].One can observe that,for MPC with MLS approximation of localized type,using a time step two orders lower than the time step used in global RBF,the absolute errors present two orders higher accuracy.
Finally,in Fig.3,the graphs of the real part and the imaginary parts of the numerical and the analytical solutions using MLS are shown at timet=1,withdx=dy=0.1,dt=0.05.Note that there is no essential divergence between the exact solution and the numerical solution in Fig.2,for the given accuracy.
Example 4
Finally,we consider the generalized nonlinear two-dimensional Schr?dinger equation written as[Dehghan,and Mirzaei(2008)]:
with the initial and boundary conditions
ψ(x,y,0)=cos(x)cos(y),(x,y)∈?
and Neumann boundary conditions on all sides of the spatial domain
Table 6:Maximum absolute error of multiquadrics and thin plate spline-based scheme at different times with dx=dy=0.1,dt=0.0005 and c=0.45 for MQ.For every value of t,the first and second rows of data correspond to the use of MQ and TPS as the radial basis function,respectively and the third for the MPC when dx=dy=0.1,dt=0.05.
Figure 3:Plots of the exact and the numerical solution at t=1.0.
The analytical solution is given as
ψ(x,y,t)=e?itcos(πx)cos(πy).
The lagging of coefficients method has been utilized to eliminate the non-linearity of the examined problem. The spatial domain of the problem is defined as0≤x,y≤1.The function used in the present problem are defined asC(x,y)=1?2π2,B(x,y)=?1?2π2??1?cos2(πx)cos2(πy)?andp=2.We have to notice that the accuracy of the case under consideration agrees with the exact solution at about two signifi-cant digits and, as the time increases it becomes worse. This is due to the imposition of the Neumann boundary conditions.When using Dirichlet boundary conditions the accuracy of the numerical results increases.Following the aforementioned procedure the final linearized system in matrix notation can be written as
Figure 4:Analytical and numerical solutions at various time.
In the present work we used the meshless numerical scheme to solve the two dimensional time-dependent linear and nonlinear Schr?dinger equation using the point collocation method with MLS approximation.For the Schr?dinger equation we developed a fully coupled,transient,and strong-form solver for the real and the imaginary parts of the general solution of the so-called quantum hydrodynamic(QHD)equation.The proposed scheme is applied to four benchmark cases having analytical solutions,with our results exhibiting excellent agreement with all the analytical ones.The numerical results were also compared with those provided by another collocation method,that is,the global Radial Basis Function method.The numerical results provided by the proposed scheme are highly accurate,compared with the ones provided by the multiquadrics and the thin plates splines RBF.Furthermore,in some cases they are also less CPU time and memory consuming.This makes the application of the MLS approximation very attractive for the numerical solution of this kind of physical problems.
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