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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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