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One might expect that, if there exist Szegő style recurrence relations for the reproducing kernels, then it should be possible to derive recurrence relations in the Szegő style for the orthogonal functions themselves. However, deriving these is not as simple as for the reproducing kernels, in the sense that the transition matrices that give the recurrence are not precisely J-unitary, but it is still possible to get some recurrences that coincide with the Szegő recurrence in the polynomial case. This will be done in the first section of this chapter.
Related to this recurrence are the so-called functions of the second kind. They are also solutions of the same recurrence but with different initial conditions. Because they will be important in obtaining several interpolation properties, we shall study them in some detail in Section 4.2.
General solutions of the recurrence, which are linear combinations of first and second kind functions, are then treated in Section 4.3 and we include there an analog of Green's formula. The latter will be used in Chapter 10 on moment problems.
Since the convergents of a continued fraction are linked by a three-term recurrence relation, there is a natural link between three-term recurrence relations and continued fractions. This is explained in Section 4.4.
Finally, Section 4.5 gives some remarks about the situation when not all the points αk are in O, but when they are arbitrarily distributed in O \ ∂O. The case where they are all on ∂O is discussed in Chapter 11.
This work deals with a system of nonlinear parabolic equations arisingin turbulence modelling. The unknowns are the N components of the velocityfield u coupled with two scalar quantities θ and φ. The systempresents nonlinear turbulent viscosity $A(\theta,\varphi)$ and nonlinearsource terms of the form $\theta^2|\nabla u|^2$ and $\theta\varphi|\nabla u|^2$ lying in L1. Some existence results are shown in this paper, including$L^\infty$-estimates and positivity for both θ and φ.
We show that Boltzmann's collision operator can be written explicitlyin divergence and double divergence forms. These conservativeformulations may be of interest for both theoretical and numericalpurposes. We give an application to the asymptotics of grazing collisions.
This note deals with the approximation, by a P1 finite element method with numerical integration,of solution curves of a semilinear problem. Because of both mixed boundary conditions and geometrical properties of the domain, some of the solutions do not belong to H2. So, classical results for convergence lead to poor estimates. We show how to improve such estimates with the use of weighted Sobolev spaces together with a mesh“a priori adapted” to the singularity. For the H1 or L2-norms,we achieve optimal results.
The initial-boundary value problem of two-dimensionalincompressible fluid flow in stream function form is considered.A prediction-correction Legendre spectral scheme is proposed, which iseasy to be performed.The numerical solution possesses the accuracy of second-order in time and higher order in space. Thenumerical experiments show the high accuracy of this approach.
In this paper, a multi-parameter error resolutiontechnique is applied into a mixed finite element method for theStokes problem. By using this technique and establishing a multi-parameter asymptotic error expansion for the mixed finite element method, an approximation of higheraccuracy is obtained by multi-processor computers in parallel.
We prove existence (uniqueness is easy) of a weak solution to a boundary value problem for an equation like $(v-1)^+_t = v_{xx} + F(v)_x$ where the function $F: \Bbb R\rightarrow\Bbb R$ is onlysupposed to be locally lipschitz continuous. In order to replace the lack of compactness in t on v<1, we use nonlinear semigroup theory.
We propose a two point subdivision scheme with parameters to draw curves that satisfy Hermite conditions at both ends of [a,b]. We build three functions f,p and s on dyadic numbers and, using infinite products of matrices, we prove that, under assumptions on the parameters, these functions can be extended by continuity on [a,b], with f'=p and f''=s .
The Navier–Stokes equations are approximated by means ofa fractional step, Chorin–Temam projection method; the time derivativeis approximated by a three-level backward finite difference, whereasthe approximation in space is performed by a Galerkin technique.It is shown that the proposed scheme yields an errorof ${\cal O}(\delta t^2 + h^{l+1})$for the velocity in the norm of l2(L2(Ω)d), where l ≥ 1 isthe polynomial degree of the velocity approximation. It is also shownthat the splitting error of projection schemes based on theincremental pressure correction is of ${\cal O}(\delta t^2)$ independent of theapproximation order of the velocity time derivative.
We give results for the approximation of a laminate withvarying volume fractions for multi-well energy minimizationproblems modeling martensitic crystals thatcan undergo either an orthorhombicto monoclinic or a cubic to tetragonal transformation. We construct energy minimizing sequences of deformations which satisfythe corresponding boundary condition, and we establish a series of error bounds in terms of the elastic energyfor the approximation of the limiting macroscopicdeformation and the simply laminated microstructure.Finally, we give results for the corresponding finite element approximation of the laminate with varying volume fractions.
In this paper, we study some finite volume schemes for the nonlinear hyperbolic equation ${u_t}(x,t)+\mbox{div}F(x,t,u(x,t))=0$ with the initial condition $u_{0}\in{L^\infty}(\mathbb{R}^N)$. Passing to the limit in these schemes, we prove the existence of an entropy solution $u\in{L^infty}(\mathbb{R}^N\times\mathbb{R}_+)$. Proving also uniqueness, we obtain the convergence of the finite volume approximation to the entropy solution in $L^p_{loc}(\mathbb{R}^N\times\mathbb{R}_+)$, 1 ≤ p ≤ +∞. Furthermore, if ${u_0}\in {L^\infty}\cap\mbox{BV}_{loc}(\mathbb{R}^N)$, we show that $u\in\mbox{BV}_{loc}(\mathbb{R}^N\times\mathbb{R}_+)$, which leads to an “$h^{\frac{1}{4}}$” error estimate between the approximate and the entropy solutions (where h defines the size of the mesh).
In this paper we present a novel exponentially fitted finite elementmethod with triangular elements for the decoupled continuity equations in the drift-diffusion model of semiconductor devices.The continuous problem is first formulated as a variational problem using a weighted inner product. A Bubnov-Galerkinfinite element method with a set of piecewise exponential basis functions is then proposed. The method is shown to be stable and can be regarded asan extension to two dimensions of the well-known Scharfetter-Gummel method.Error estimates for the approximate solution and its associated flux are given. These h-order error bounds depend on some first-order seminorms of the exact solution, the exact fluxand the coefficient function of the convection terms.A method is also proposed for the evaluation of terminal currentsand it is shown that the computed terminal currents are convergent andconservative.
Lagrangian and augmented Lagrangian methods for nondifferentiableoptimization problems that arise from the total bounded variation formulation of image restoration problems are analyzed. Conditional convergence of theUzawa algorithm and unconditional convergence of the first order augmentedLagrangian schemes are discussed. A Newton type method based on an activeset strategy defined by means of the dual variables is developed andanalyzed. Numerical examples for blocky signals and images perturbedby very high noise are included.
In this paper we consider the numerical computation of the optimal costfunction associated to the problem that consists in finding the minimum ofthe maximum of a scalar functional on a trajectory. We present anapproximation method for the numerical solution which employs bothdiscretization on time and on spatial variables. In this way, we obtain afully discrete problem that has unique solution. We give an optimal estimatefor the error between the approximated solution and the optimal costfunction of the original problem. Also, numerical examples are presented.
A hush descended over the classroom as Inspector McGee strode to the podium. After all, he had served on the Fraud Squad for over 20 years, and the talks that he gave to each year's crop of police recruits were the stuff of legend. No one else had the fund of stories about past experiences mat he did. Each year he amazed the rookies by telling them of yet another bizarre technique mat he had used to unmask the schemes of the city's con artists. It seemed that there was no branch of knowledge that he hadn't exploited at some point in his career. But this year, the rumor went, he was going to outdo himself; somehow he had actually used calculus to convict a criminal! It seemed hard to believe. The rookies strained forward in anticipation.
“First of all, I'd like to thank the Chief for giving me a chance to talk to you young recruits,” McGee began. “My goal today is to convince you that you must always be ready to use experts to help you get to the bottom of a fraud scheme. In fact, in one of my most interesting cases I called on the smarts of a bunch of young people about the same age as you. Let me tell you about it.
“A few years ago a new bar opened in the Little Bohemia district—maybe you remember it. Upstairs it featured the usual assortment of rock bands, but the real attraction was in the basement. They called it Luigi's Lizard Room, and judging from the sleazy characters that hung out there, it was well-named. It was full of pool tables—beautiful, big tables with lots of room between them and well-enough lit so that you could see what you were doing.
Topic: Required launch velocity of LS50 quasion probe rockets for meteor interception
This report addresses the calculation of the launch velocity of the rocket fired from Lunar Station 50 at 3:00 PM on July 21, 21xy, to intercept the meteor on a collision course with Lunar Station Alpha.
Let R denote the radius of Xzyqgon (all distances will be measured in km). Let d denote the distance from Lunar Station 50 (henceforth denoted LS50) to the meteor at 3 PM. Let u denote the speed of the meteor (all speeds in km/sec), and let v denote the maximum possible speed at which the research rockets can be launched.
The situation at 3 PM is shown in Figure A. The circle is the “great circle” on Xzyqgon on which both LS50 and Lunar Station Alpha (henceforth abbreviated LSα) sit. Referring to Figure A, M is the location of the meteor, N is the North Pole where LSα is located, F is the location of LS50, and O is the center of Xzyqgon. Finally, P is the intersection of the path of the research rocket and the path of the meteor, and Q is where the great circle through LS50 and LSα meets the Equator.