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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