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Numerical investigation of vortex breakdown on a delta wing

Author
AGRAWAL, S; BARNETT, R. M; ROBINSON, B. A
McDonnell Douglas Corp., Saint Louis MO 63166, United States
Source

AIAA journal. 1992, Vol 30, Num 3, pp 584-591 ; ref : 27 ref

CODEN
AIAJAH
ISSN
0001-1452
Scientific domain
Aeronautics astronautics; Mechanics acoustics; Transportation
Publisher
American Institute of Aeronautics and Astronautics, Reston, VA
Publication country
United States
Document type
Article
Language
English
Keyword (fr)
Aile delta Aérodynamique Bord fuite Eclatement Ecoulement tourbillonnaire Plaque plane Simulation numérique Tourbillon
Keyword (en)
Delta wing Aerodynamics Trailing edge Bursting Swirling flow Flat plate Numerical simulation Vortex
Keyword (es)
Ala delta Aerodinámica Borde salida Estallido Flujo torbellinal Placa plana Simulación numérica Torbellino
Classification
Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G85 Applied fluid mechanics / 001B40G85B Aerodynamics

Discipline
Physics : fluid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
5153332

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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