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Titlebook: Computational Science and Its Applications – ICCSA 2020; 20th International C Osvaldo Gervasi,Beniamino Murgante,Yeliz Karaca Conference pr

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31#
發(fā)表于 2025-3-27 00:05:06 | 只看該作者
32#
發(fā)表于 2025-3-27 03:59:10 | 只看該作者
A Convergence Analysis of a Multistep Method Applied to an Advection-Diffusion Equation in 1-Dlas. The present study discusses the convergence of the method when applied to a convection-diffusion equation in 1-D. The convergence analysis conducted produced sufficient conditions for the consistency analysis and used the von Neumann analysis to demonstrate that the method is stable. Moreover,
33#
發(fā)表于 2025-3-27 08:36:07 | 只看該作者
The Influence of Reordering Algorithms on the Convergence of a Preconditioned Restarted GMRES Method preconditioned by three ILU-type preconditioners. This paper investigates the effect of 13 orderings on the convergence of the preconditioned GMRES solver restarted every 50 steps when applied to nine real large-scale nonsymmetric and not positive definite matrices. Specifically, this paper shows t
34#
發(fā)表于 2025-3-27 13:16:36 | 只看該作者
35#
發(fā)表于 2025-3-27 15:16:40 | 只看該作者
User-Friendly Expressions of the Coefficients of Some Exponentially Fitted Methodsllations and loss of precision. Usually the coefficients of an EF method are expressed in terms of ., where . is the frequency and . is the step size. Often, these coefficients exhibit a 0/0 indeterminate form when .. To avoid this feature we will use two sets of functions, called . and ., which hav
36#
發(fā)表于 2025-3-27 18:01:47 | 只看該作者
CFD Prediction of Retractable Landing Gear Aerodynamicshe mean flow around the landing-gear system including doors is simulated by using the Reynolds-averaged Navier-Stokes modelling approach, the governing equations being solved with a finite volume-based numerical technique. The computational grid is automatically adapted to the time-changing geometry
37#
發(fā)表于 2025-3-27 23:45:21 | 只看該作者
CFD Prediction of Aircraft Control Surfaces AerodynamicsThe virtual experiments are performed in operational conditions by resolving the mean turbulent flow field around a suitable model of the whole aircraft. The Reynolds-averaged Navier-Stokes modelling approach is used, where the governing equations are solved with a finite volume-based numerical tech
38#
發(fā)表于 2025-3-28 02:48:12 | 只看該作者
39#
發(fā)表于 2025-3-28 06:19:17 | 只看該作者
Bounds for Complete Arcs in , and Covering Codes of Radius 3, Codimension 4, Under a Certain Probabis the smallest length of a .-ary linear code of codimension (redundancy) ., covering radius ., and minimum distance?.; in particular, . is the smallest length . of an . quasi-perfect MDS code. By the definitions, .. In this paper, a step-by-step construction of complete arcs in . is considered. It i
40#
發(fā)表于 2025-3-28 11:57:36 | 只看該作者
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