Orbital stability of solitary waves for the Klein-Gordon-Zakharov equations

1.IntroductionInthetheoreticalinvestigationsofthedynamicsofstrongLangmuirturbulenceinplasmaphysics,varioustypesofZakharovequationstakeanimportantrole(see[3--8]).Intillspaper,weconsiderthefollowingKlein-Gordon-Zakharovequations:{:ti:::::;.;;:~"aiR,(11)withuacomplexfunctionandnarealfunction.Thelocalandglobalekistenceoftheinitialvalueproblemfor(1.l)wasconsideredin[4,6].Inthispaper,weconsidertheorbitalstabilityofthesolitarywavesof(1.l).Byapplyingtheabstracttheoryof[1,2]anddetailedspectralanalys…     

平均样本间隔的性质及其在拍卖中的应用

研究了平均样本间隔E(Xk+1:n-Xk:n)的性质.证明了当X具有DRHR年龄性质时,E(Xk+1:n-Xk:n)关于样本容量n递减.而当X具有IFR年龄性质时,E(Xk+1:n-Xk:n)-E(Xk+2:n+1-Xk+1:n+1)非负.最后,讨论了主要结果在拍卖模型中的应用.     

平方差公式的妙用

平方差公式 o,一去,卿(。+‘)(a一b)是大家安硒的.这里我们介绍它在一类数列的求和与承积中的妙用. 翻1求:+s+…+(:。+一)(”〔N)的值. 筋:.,”+r.〔(。+z)阵,〕·z .〔(人+一)+。〕·〔(n+一)一,) .(”+J)一。吕. .’.原式.(2,一1)+(少一2“)+…+(。十1),一丹‘. .”‘+2”.例生求扣卜l1.·…(”一‘+1汹你娜2二(企二一1,(21+一、(:,一r)2:’一’十1二一、.2里 2忿一1一1原式二(2:+一)(2:+z)(:。+1)…(2:‘一‘+i) l忿2:一l夕攀一l一1—一’“”’一二f-22一1 .2 似上解法,的差积变形上. 二、.二一之.妙在何处釜妙就妙在刊用平方差公式例l…     

波动方程解的渐近性态的一个注记

号1.引言在Q=(0,印)x口内,=0,(1 .1)(1 .2)u:}:之。=功(x)(1 .3)解的渐近性态.其中口为R”中具有光滑边界a口的有界区域,入>o为常数.令U二(。,v),,。=“:,则上述问题可改写为如下形式: AU=O,有Q内,(1 .4) 入v}。o=0,(1 .5)“(甲,劝)戈1 .6)丝次巫如叭 .﹃t!万..JI 一O其中A= 0一A 当口的边界O口由两部分厂。,厂:组成,在厂,上给定形如(1 .2)的边界条件,而在厂。上给定Diriehlet型的边界条件u}:。二o时,J.P.Quinn与D.L.Russell〔1〕证明了当t”co时,问题(1 .1)一(1 .3)的解趋向于零.稍后,G.Chen在关于区域口的进一步假设下,证明了这…     

综合题新编选登

题139数列{an}满足:a1=a(a>2),且an≥an2-1na n2-1n-1(n≥2,n∈N*).求证:1)an≥(n-21n)aa 2;2)a1.a2.a3.….an>n2!.证1)a1=a>2>0,易知an>0.将条件an≥an2-1na n2-1n-1变形,得:2ann-2ann--11≤1,于是有:2a22-a21≤1,2a33-2a22≤1,…,2ann-2ann--11≤1,上述诸式相加得:2ann-a21≤     

NUMERICAL APPROXIMATIONS OF A SEMI-LINEAR ELLIPTIC PROBLEM

1IntroductionConsidertl1eparameterdependentequationwhereA,ltERarepara1ueterandf:R-RandS:R-RaresinoothoddfunctionwithLetS1:u(x)-u(T-x),r={S1,I}then(l.1)isr-equivariant.Tl1eequality(1.2a)isjustanormalizatiolloffatx=o.Otherwise,onelllayreseektl1eparameterxtoensure(1.2a).To8implifyanalysisweintroduceaSobolevspaceX:=Hl(o,1)anddefilleamappingT:gEL'(o,T)-lL:=TgEXimp1icitly:for(Tg)'V'dx=-jorgl)dx,VvEX,aweakformof(1.1)inXxR2isDuetof(o)=O,theproblem(1.3)(resp.(1))hasatrivialsolutioncurvesC…     

A TOBIN-TYPE ESTIMATE OF CENSORED LINEAR MODELS

1IntroductionConsiderthelinearregressioumodelcensoredfromtheleft:K=m{K,0}=rnax{Z:W ei,0},1Si5n,(1.1)whereZi=(1,X:),,15i5n,7o=(ac,P6)'(1'2)ThedimensionalityofXiisd21.WeobBerve(Xi,K)',1SiSn.Basedontheseobservations,wetrytogivesomeestimationofac,ortesthypothesisonit.Themodelwasfirstconsideredbycabin[llundertheassumptionthatelfe2,''arelid.withacommonnormaldistributionN(0,rs:).HedefinedtheMLEof7o,whichnowisusuallyknownastheTobinestimator.TheconsistencyOfthisestimatorwasestablishedbyAmend…     

NON-NEGATIVE SOLUTIONS FOR A CLASS OF NON-POSITONE PROBLEMS

1IntroduInthispaperwestudyill(.)(l}xlsl(.)ll(:()noTI-1)ega,t]v(3s(>1lltionsfort,h(i1,woilo]lit,boundaryvalueproblemsu\ry;l;(:i.t>(v,>\,:t),:j:=fti-i'...ifn(j)>l),A>0isdcollstanta,f,dj'e(!'l,.,ti,fi<,,f(())<0(l.:i)111.of)i(lfllsifs{.1.l:)-(.I.2)havel,ecnsi…     

数学诡辩

1.不过圆心的弦 与直径相等题:如图:在00中,ALB是直径,D是弦AC的中点,连结BD并延长交00于E,连结cE,求证:cE~月Z孔 证明:在△滋刀刀与△五汪℃中. 乙A一乙E,匕B一艺C,乙通刀刀一艺召Z刃,月刀二货, △月刀刀望△召之兀),…月刀~C刀认五.都是根又都是增根解方程aretg(:一1) areetg(x 1)=arctg冬. 乙解1设a=aretg(:一l), 则tga一z一1.设刀一areetg(: l),则etg刀=: 1. tga十tg刀 tg(a 刀)一下共一月誓二 ,、一‘厂‘l一tga .tg声 l、1 ~tg(arctg音)一音. ,、一一,2‘2’:一1十即 1劣 1l一劣一lx 1l2 解得:一士1,经检验,知x一1是原方程的…     

上期课外练习解答

初一年级1.解’.‘1--x=丽l,1一y一志 厶UUl 厶uv厶 .‘. 1--Jc>1一y, .‘.x相似文献   

RKDG methods with WENO type limiters and conservative interfacial procedure for one-dimensional compressible multi-medium flow simulations

In this paper, we continue on studying the Runge-Kutta discontinuous Galerkin (RKDG) methods to solve compressible multi-medium flow with conservative treatment of the moving material interface. Comparing with the paper by J. Qiu, T.G. Liu and B.C. Khoo [J. Comput. Phys. 222 (2007) 353-373], we adopt the HLLC flux instead of Lax-Friedrichs numerical flux, the finite volume weighted essentially nonoscillatory (WENO) and Hermite WENO (HWENO) reconstructions as limiter instead of TVB limiter for RKDG. The HLLC flux is based on the approximate Riemann solver with little numerical viscosity and can resolve the contact discontinuity and shear wave very well. For limiter procedure, first we use the KXRCF indicator to identify the troubled cell, then apply WENO or HWENO method to reconstruct the polynomial in the troubled cell, while maintaining the cell average. This limiter procedure is more accurate and less problem dependent than the TVB limiter. Numerical results in one dimension for multi-medium flows such as gas-gas and gas-water are provided to illustrate the capability of these procedures.     

A simple weighted essentially non-oscillatory limiter for the correction procedure via reconstruction (CPR) framework on unstructured meshes

In this paper, we adapt a simple weighted essentially non-oscillatory (WENO) limiter, originally designed for discontinuous Galerkin (DG) schemes on two-dimensional unstructured triangular meshes [39], to the correction procedure via reconstruction (CPR) framework for solving nonlinear hyperbolic conservation laws on two-dimensional unstructured triangular meshes with straight or curved edges. This is an extension of our earlier work [4] in which the WENO limiter was designed for the CPR framework on regular meshes. The objective of this simple WENO limiter is to simultaneously maintain uniform high order accuracy of the CPR framework in smooth regions and control spurious numerical oscillations near discontinuities. The WENO limiter we adopt in this paper uses information only from the target cell and its immediate neighbors. Hence, it is particularly simple to implement and will not harm the conservativeness and compactness of the CPR framework. Since the CPR framework with this WENO limiter does not in general satisfy the positivity preserving property, we also extend the positivity-preserving limiters [36], [33] to the CPR framework. Numerical results for both scalar equations and Euler systems of compressible gas dynamics are provided to illustrate the good behavior of this procedure.     

An invariant‐region‐preserving limiter for DG schemes to isentropic Euler equations

In this article, we introduce an invariant‐region‐preserving (IRP) limiter for the p‐system and the corresponding viscous p‐system, both of which share the same invariant region. Rigorous analysis is presented to show that for smooth solutions the order of approximation accuracy is not destroyed by the IRP limiter, provided the cell average stays away from the boundary of invariant region. Moreover, this limiter is explicit, and easy for computer implementation. A generic algorithm incorporating the IRP limiter is presented for high order finite volume type schemes as long as the evolved cell average of the underlying scheme stays strictly within the invariant region. For high order discontinuous Galerkin (DG) schemes to the p‐system, sufficient conditions are obtained for cell averages to stay in the invariant region. For the viscous p‐system, we design both second and third order IRP DG schemes. Numerical experiments are provided to test the proven properties of the IRP limiter and the performance of IRP DG schemes.     

Implementing a discontinuous Galerkin method for the compressible,inviscid Euler equations in the DUNE framework

A discontinuous Galerkin scheme was implemented in the DUNE framework to solve the compressible, inviscid Euler equations in a multi-dimensional Cartesian grid. It uses a HLLC Riemann solver for the numerical fluxes in the interfaces, a total variation bounded limiter to handle discontinuities, a positivity preserving limiter for near vacuum conditions, and adaptive mesh refinement (AMR). (© 2014 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim)     

Logistic模型阈值控制悖论及复杂性分析

研究了Logistic模型稳态均值在阈值控制下产生反直觉变化现象与复杂响应的机理.结果表明,阈值控制能引起映射区间改变和映射分布变化,二者之间的竞争导致了受控Logistic模型稳态均值的反直觉变化现象与复杂响应.在阈值下限接近0或阈值上限接近1时,映射分布变化是影响稳态均值复杂响应的主导因素.阈值下限大于其临界值或阈值上限小于其临界值时,稳态均值变化主要由映射区间改变决定,此时,受控Logistic模型稳态均值会出现反直觉变化现象.理论分析结果通过数值仿真得到进一步证实.     

A flux-corrected transport algorithm for handling the close-packing limit in dense suspensions

Convection of a scalar quantity by a compressible velocity field may give rise to unbounded solutions or nonphysical overshoots at the continuous and discrete level. In this paper, we are concerned with solving continuity equations that govern the evolution of volume fractions in Eulerian models of disperse two-phase flows. An implicit Galerkin finite element approximation is equipped with a flux limiter for the convective terms. The fully multidimensional limiting strategy is based on a flux-corrected transport (FCT) algorithm. This nonlinear high-resolution scheme satisfies a discrete maximum principle for divergence-free velocities and ensures positivity preservation for arbitrary velocity fields. To enforce an upper bound that corresponds to the maximum-packing limit, an FCT-like overshoot limiter is applied to the converged convective fluxes at the end of each time step. This postprocessing step imposes an additional physical constraint on the numerical solution to the unconstrained mathematical model. Numerical results for 2D implosion problems illustrate the performance of the proposed limiting procedure.     

On the optimization of flux limiter schemes for hyperbolic conservation laws

A classic strategy to obtain high‐quality discretizations of hyperbolic partial differential equations is to use flux limiter (FL) functions for blending two types of approximations: a monotone first‐order scheme that deals with discontinuous solution features and a higher order method for approximating smooth solution parts. In this article, we study a new approach to FL methods. Relying on a classification of input data with respect to smoothness, we associate specific basis functions with the individual smoothness notions. Then, we construct a limiter as a linear combination of the members of parameter‐dependent families of basis functions, and we explore the possibility to optimize the parameters in interesting model situations to find a corresponding optimal limiter. © 2012 Wiley Periodicals, Inc. Numer Methods Partial Differential Eq, 2013     

On third-order limiter functions for finite volume methods

In this article, we propose a finite volume limiter function for a reconstruction on the three-point stencil. Compared to classical limiter functions in the MUSCL framework, which yield 2^nd-order accuracy, the new limiter is 3^rd-order accurate for smooth solution. In an earlier work, such a 3^rd-order limiter function was proposed and showed successful results [2]. However, it came with unspecified parameters. We close this gap by giving information on these parameters.     

A selection limiter of DSMC for near continuum flows

A selection limiter for the direct simulation monte carlo (DSMC) method is proposed to simulate near continuum flows. The selection limiter is calculated according to a continuum breakdown parameter and is used to limit the number of potential collision pairs. A Couette flow, a supersonic flow into a pitot probe and a nozzle plume flow are studied and compared with the standard DSMC to validate present method. It is found that its computational cost is about 35% of that of the standard DSMC method with satisfactory accuracy in the near continuum regime.     

An Exact Riemann Solver for a Fluidized Bed Model

We study a 2 x 2 hyperbolic system of conservation laws withsource term arising in a fluidized bed model. The system issolved numerically and results are presented to demonstratethe occurrence of ‘slugging’ in the full model equations.The numerical procedure is based on operator splitting and Godunov'smethod, for which we derive the exact solution of the Riemannproblem. A second-order improvement due to Davis (1988) mayproduce small oscillations near shocks and these can be reducedif the underlying flux limiter of the Davis method is replacedby the minmod limiter.