𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Use of central-difference operators for solution of singularly perturbed problems

✍ Scribed by Hegarty, Alan F. ;Miller, John J. H. ;O'Riordan, Eugene ;Shishkin, G. I.


Publisher
John Wiley and Sons
Year
1994
Tongue
English
Weight
320 KB
Volume
10
Category
Article
ISSN
1069-8299

No coin nor oath required. For personal study only.

✦ Synopsis


Singularly perturbed second-order elliptic equations with boundary layers are considered. These may be considered as model problems for the advection of some quantity such as heat or a pollutant in a flow field or as linear approximations to the Navier-Stokes equations for fluid flow. Numerical methods composed of central-difference operators on special piece-wise-uniform meshes are constructed for the above problems. Numerical results are obtained which show that these methods give approximate solutions with error estimates that are independent of the singular perturbation parameter. An open theoretical problem is posed.


πŸ“œ SIMILAR VOLUMES


Difference schemes for the class of sing
✍ Ismail R. Rafatov; Sergey N. Sklyar πŸ“‚ Article πŸ“… 2004 πŸ› John Wiley and Sons βš– 124 KB πŸ‘ 2 views

## Abstract This work deals with the construction of difference schemes for the numerical solution of singularly perturbed boundary value problems, which appear while solving heat transfer equations with spherical symmetry. The projective version of integral interpolation (PVIIM) method is used. De

Structure of nontrivial nonnegative solu
✍ Zhengce Zhang; Zongming Guo πŸ“‚ Article πŸ“… 2007 πŸ› John Wiley and Sons 🌐 English βš– 238 KB

## Abstract We study structure of nontrivial nonnegative solutions for a class of singularly perturbed quasilinear Dirichlet problems. It is shown that there are infinitely many least‐energy solutions and they are spike‐layer solutions. Moreover, the measure of each spike‐layer is estimated as the

Fast suboptimal solution to the static o
✍ Dj. Petkovski; N. Harkara; Z. Gajic πŸ“‚ Article πŸ“… 1991 πŸ› Elsevier Science 🌐 English βš– 314 KB

Airliner--The reduced-order suboptimal solution to the static output control problem of linear singularly perturbed system is obtained in terms of the fast variables only, assuming the special structure of initial conditions for the slow and fast variables. The problem of big initial conditions of t