A DETAILED STUDY OF ATTACHED AND SEPARATED COMPRESSION CORNER FLOWFIELDS IN HIGH REYNOLDS NUMBER SUPERSONIC FLOW
- Author
- SETTLES GS; FITZPATRICK TJ; BOGDONOFF SM
PRINCETON UNIV. MECH. AEROSPACE ENG. DEP., PRINCETON NJ, USA - Source
- AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS FLUID AND PLASMA DYNAMIC CONFERENCE. 11/1978/SEATTLE WA; USA; NEW YORK: AIAA; DA. 1978; 78-1167; 9 P.; BIBL. 21 REF.
- Document type
- Conference Paper
- Language
- English
- Keyword (fr)
- ECOULEMENT SUPERSONIQUE DECOLLEMENT ECOULEMENT ETUDE EXPERIMENTALE COUCHE LIMITE TURBULENTE ANGLE VISUALISATION DISTRIBUTION PRESSION DISTRIBUTION VITESSE FROTTEMENT SUPERFICIEL MECANIQUE FLUIDE
- Keyword (en)
- SUPERSONIC FLOW FLOW SEPARATION EXPERIMENTAL STUDY TURBULENT BOUNDARY LAYER ANGLE VISUALIZATION PRESSURE DISTRIBUTION VELOCITY DISTRIBUTION SKIN FRICTION 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
- PASCAL7930362277
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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