Implicit High-Order Spectral Finite Volume Method for Inviscid Compressible Flows-Reference-Cited by-同舟云学术

Implicit High-Order Spectral Finite Volume Method for Inviscid Compressible Flows

Published:2010-10 Issue:10 Volume:48 Page:2365-2376
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Breviglieri Carlos¹,Azevedo Joao Luiz F.²,Basso Edson²,Souza Maximiliano A. F.¹

Affiliation:

1. Instituto Tecnologico de Aeronautica, 12228-900 Sao Jose dos Campos, Sao Paulo, Brazil

2. Instituto de Aeronautica e Espaco, 12228-903 Sao Jose dos Campos, Sao Paulo, Brazil

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J050395

Reference36 articles.

1. Scalabrin, L. C. "Numerical Simulation of Three-Dimensional Flows over Aerospace Configurations," M.S. Thesis, Instituto Tecnológico de Aeronáutica,São Josédos Campos, SP,Brazil, 2002.

2. Chimera Simulations of Supersonic Flows over a Complex Satellite Launcher Configuration

3. Flux-vector splitting for the Euler equations

4. A Sequel to AUSM: AUSM+

5. Approximate Riemann solvers, parameter vectors, and difference schemes

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