| Texto completo | |
| Autor(es): |
Carlos Junqueira-Junior
[1]
;
Leonardo Costa Scalabrin
[2]
;
Edson Basso
[3]
;
João Luiz F. Azevedo
[4]
Número total de Autores: 4
|
| Afiliação do(s) autor(es): | [1] Instituto Tecnológico de Aeronáutica - Brasil
[2] EMBRAER S.A. - Brasil
[3] Instituto de Aeronáutica e Espaço - Brasil
[4] Instituto de Aeronáutica e Espaço - Brasil
Número total de Afiliações: 4
|
| Tipo de documento: | Artigo Científico |
| Fonte: | J. Aerosp. Technol. Manag.; v. 6, n. 3, p. 267-280, 2014-09-00. |
| Resumo | |
ABSTRACT: The work is a study of conservation on linearization techniques of time-marching schemes for the unstructured finite volume Reynolds-averaged Navier-Stokes formulation. The solver used in this work calculates the numerical flux applying an upwind discretization based on the flux vector splitting scheme. This numerical treatment results in a very large sparse linear system. The direct solution of this full implicit linear system is very expensive and, in most cases, impractical. There are several numerical approaches which are commonly used by the scientific community to treat sparse linear systems, and the point-implicit integration was selected in the present case. However, numerical approaches to solve implicit linear systems can be non-conservative in time, even for formulations which are conservative by construction, as the finite volume techniques. Moreover, there are physical problems which strongly demand conservative schemes in order to achieve the correct numerical solution. The work presents results of numerical simulations to evaluate the conservation of implicit and explicit time-marching methods and discusses numerical requirements that can help avoiding such non-conservation issues. (AU) | |
| Processo FAPESP: | 13/21535-0 - Simulação de grandes escalas e aeroacústica de jatos supersônicos perfeitamente expandidos |
| Beneficiário: | Sami Yamouni |
| Modalidade de apoio: | Bolsas no Brasil - Pós-Doutorado |