Computation of aerodynamic load and coefficient for satellite launch vehicle
- Author
- MEHTA, R. C1 ; SASTRY, M. S1
[1] Aerodynamics Division, Vikram Sarabhai Space Centre, Trivandrum 695 022, India - Source
Indian journal of engineering & materials sciences. 1997, Vol 4, Num 2, pp 41-48 ; ref : 8 ref
- ISSN
- 0971-4588
- Scientific domain
- Chemical engineering; Civil engineering; Mechanical engineering; Metallurgy, welding
- Publisher
- Council of Scientific & Industrial Research, New Delhi
- Publication country
- India
- Document type
- Article
- Language
- English
- Keyword (fr)
- Distribution pression Distribution vitesse Ecoulement axisymétrique Ecran thermique Equation Euler Fluide compressible Fluide non visqueux Force aérodynamique Fusée Lancement Méthode volume fini Simulation numérique Spationef
- Keyword (en)
- Pressure distribution Velocity distribution Axially symmetric flow Thermal shields Euler equations Compressible fluid Non viscous fluid Aerodynamic force Rockets Launching Finite volume method Numerical simulation Spacecraft
- Keyword (es)
- Distribución presión Flujo axisimétrico Fluido compresible Fluido no viscoso Fuerza aerodinámica Método volumen finito Simulación numérica Vehículo espacial
- 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
- Discipline
- Physics : fluid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 2729874
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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