Effect of artificial viscosity on three-dimensional flow solutions
- Author
- ELI TURKEL1 ; VATSA, V. N
[1] Tel-Aviv univ., Tel-Aviv, Israel - Source
AIAA journal. 1994, Vol 32, Num 1, pp 39-45 ; ref : 14 ref
- CODEN
- AIAJAH
- ISSN
- 0001-1452
- Scientific domain
- Aeronautics astronautics; Mechanics acoustics; Transportation
- Publisher
- American Institute of Aeronautics and Astronautics, Reston, VA
- Publication country
- United States
- Document type
- Article
- Language
- English
- Keyword (fr)
- Aile Dissipation visqueuse Distribution pression Ecoulement transsonique Frottement superficiel Modélisation Onde choc Simulation numérique Méthode volume fini
- Keyword (en)
- Wing Viscous dissipation Pressure distribution Transonic flow Skin friction Modeling Shock waves Numerical simulation Finite volume method
- Keyword (es)
- Ala Disipación viscosa Distribución presión Frotamiento superficial Modelización Simulación numérica Método volumen finito
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G11 Computational methods in fluid dynamics
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G40 Compressible flows; shock and detonation phenomena / 001B40G40H Transonic flows
- Pacs
- 4740H Transonic flows
- Discipline
- Physics : fluid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 3873502
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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DOI
10.2514/3.11948 
https://dx.doi.org/10.2514/3.11948
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