Iteration strategy for upwind/relaxation solutions to the thin-layer Navier-Stokes equations
- Author
- NEWSOME, R. W; WALTERS, R. W; THOMAS, J. L
Air force Wright aeronautical lab., Wright-Patterson AFB OH, United States - Conference name
- AIAA computational fluid dynamics conference. 8 (Honolulu 1987)
- Source
AIAA journal. 1989, Vol 27, Num 9, pp 1165-1166, 2 p ; ref : 3 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
- Conference Paper
- Language
- English
- Keyword (fr)
- Algorithme Corps immergé Couche mince Ecoulement supersonique Equation Navier Stokes Forme elliptique Méthode itérative Méthode numérique Méthode relaxation
- Keyword (en)
- Algorithm Immersed body Thin film Supersonic flow Navier Stokes equation Elliptical shape Iterative method Numerical method Relaxation method
- Keyword (es)
- Algoritmo Cuerpo inmergido Capa fina Flujo supersónico Ecuación Navier Stokes Forma elíptica Método iterativo Método numérico Método relajación
- Classification
- 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
- Discipline
- Physics : fluid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 19281337
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
10.2514/3.10241 
https://dx.doi.org/10.2514/3.10241
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