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Pneumatic flow control studies using steady blowing on a supercritical aerofoil

Author
WONG, C1 ; KONTIS, K1
[1] Aero-Physics Laboratory School of Mechanical, Aerospace and Civil Engineering University of Manchester, Manchester, United Kingdom
Source

Aeronautical Journal. 2009, Vol 113, Num 1139, pp 53-63, 11 p ; ref : 21 ref

CODEN
AENJAK
ISSN
0001-9240
Scientific domain
Aeronautics astronautics; Mechanics acoustics
Publisher
Royal Aeronautical Society, London
Publication country
United Kingdom
Document type
Article
Language
English
Keyword (fr)
Anémomètre fil chaud Bord fuite Commande pneumatique Commande écoulement Couche limite Effet Coanda Etude expérimentale Force aérodynamique Installation essai Profil aérodynamique Sillage Soufflage 4762 4785G
Keyword (en)
Hot wire anemometers Trailing edge Pneumatic control Flow control Boundary layers Coanda effect Experimental study Aerodynamic force Test facilities Airfoils Wakes Blowing
Keyword (es)
Borde salida Mando neumático Efecto Coanda Fuerza aerodinámica Soplado
Classification
Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G62 Flow control

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
21039948

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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