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AGREEMENT OF HIGH CONICAL FLOW THEORY WITH EXPERIMENTAL RESULTS FOR SUPERSONIC FLOW

Author
NASTASE A
RWTH AACHEN, LEHRGEBIET AERODYNAM. FLUGES/AACHEN 5100/DEU
Source
Z. ANGEW. MATH. MECH.; ISSN 0044-2267; DDR; DA. 1980; VOL. 60; NO 7; PP. T199-T201; BIBL. 8 REF.
Document type
Article
Language
English
Keyword (fr)
AERODYNAMIQUE AILE DELTA ECOULEMENT SUPERSONIQUE ECOULEMENT CONIQUE COUCHE LIMITE COUCHE LIMITE TRIDIMENSIONNELLE OPTIMISATION
Keyword (en)
AERODYNAMICS DELTA WING SUPERSONIC FLOW CONICAL FLOW BOUNDARY LAYER THREE DIMENSIONAL BOUNDARY LAYER OPTIMIZATION
Classification
Pascal
001 Exact sciences and technology / 001B Physics

Discipline
Theoretical physics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
PASCAL8130202462

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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