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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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