A DIRECT METHOD FOR COMPUTING THE STEADY FLOW AT MACH NUMBER ONE PAST A GIVEN WING AIRFOIL
- Author
- EUVRARD D; TOURNEMINE G
DEP. MATH. INF., UNIV. RENNES, FR. - Source
- LECTURE NOTES PHYS.; GERM.; DA. 1973; NO 19; PP. 146-152; BIBL. 8 REF.; (PROC. 3RD. INT. CONF. NUMER. METHODS FLUID MECH. II. PROBL. FLUID MECH.; PARIS; 1972)
- Document type
- Conference Paper
- Language
- English
- Keyword (fr)
- AERODYNAMIQUE TRANSSONIQUE ECOULEMENT TRANSSONIQUE PROFIL AERODYNAMIQUE ECOULEMENT STATIONNAIRE METHODE NUMERIQUE PROFIL CONVEXE MECANIQUE SOLIDE MECANIQUE FLUIDE
- Keyword (en)
- SOLID MECHANICS FLUID MECHANICS
- Keyword (es)
- MECANICA DE LOS SOLIDOS MECANICA DELOS FLUIDOS
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics
- Discipline
- Theoretical physics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- PASCAL7313012723
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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