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CALCUL D'UNE TUYERE SUPERSONIQUE OU HYPERSONIQUE DE REVOLUTION.

Author
SCIBILIA MF
Source
CNRS-LAB. AEROTHERM.-529; FR.; DA. 1977; PP. (29P.); H.T. 3; ABS. ANGL.; BIBL. 7 REF.
Document type
Report
Language
French
Keyword (fr)
TUYERE ECOULEMENT SUPERSONIQUE ECOULEMENT HYPERSONIQUE TUYERE AXISYMETRIQUE METHODE CALCUL FORME GEOMETRIQUE PROGRAMME ORDINATEUR MECANIQUE FLUIDE
Keyword (en)
TUYERE SUPERSONIC FLOW HYPERSONIC FLOW AXIALLY SYMMETRIC NOZZLE CALCULATING METHOD GEOMETRICAL SHAPE COMPUTER PROGRAMS FLUID MECHANICS
Keyword (es)
MECANICA DELOS FLUIDOS
Classification
Pascal
001 Exact sciences and technology / 001B Physics

Discipline
Theoretical physics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
PASCAL7730323092

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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