INFLUENCE DE LA COURBURE TRANSVERSALE DE LA SURFACE INFERIEURE SUR LE CHAMP DE L'ECOULEMENT SUPERSONIQUE CONIQUE D'UN AVION A AILES DELTA
- Author
- KOSYKH AP; MINAJLOS AN
MOSKVA, SUN - Source
- IZVEST. AKAD. NAUK S.S.S.R., MEKH. ZHIDKOSTI GAZA; SUN; DA. 1978; NO 3; PP. 103-110; BIBL. 13 REF.
- Document type
- Article
- Language
- Russian
- Keyword (fr)
- ECOULEMENT SUPERSONIQUE FLUIDE NON VISQUEUX CORPS IMMERGE CONE AVION AILE DELTA COURBURE AERODYNAMIQUE
- Keyword (en)
- SUPERSONIC FLOW NON VISCOUS FLUID IMMERSED BODY CONE AIRPLANE DELTA WING CURVATURE AERODYNAMICS
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics
- Discipline
- Theoretical physics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- PASCAL7930145842
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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