The development of new aeronautic projects require accurate and ef®cient simulations of compressible ¯ows in complex geometries. It is well known that most ¯ows of interest are at least locally turbulent and that the modelling of this turbulence is critical for the reliability of the computations. A
✦ LIBER ✦
An edge based stabilized finite element method for solving compressible flows: formulation and parallel implementation
✍ Scribed by Azzeddine Soulaimani; Yousef Saad; Ali Rebaine
- Publisher
- Elsevier Science
- Year
- 2001
- Tongue
- English
- Weight
- 814 KB
- Volume
- 190
- Category
- Article
- ISSN
- 0045-7825
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