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Investigation of High-Lift Mechanisms for a Flat-Plate Airfoil Undergoing Small-Amplitude Plunging Oscillations

Author
CLEAVER, D. J1 ; WANG, Z1 ; GURSUL, I1
[1] University of Bath, Bath, England BA2 7AY, United Kingdom
Source

AIAA journal. 2013, Vol 51, Num 4, pp 968-980, 13 p ; ref : 22 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)
Aérodynamique Bord attaque Etude expérimentale Installation essai Mesure vitesse Plaque plane Profil oscillant Robot mobile Robotique Tourbillon Véhicule aérien inhabité Vélocimétrie image particule 4785G
Keyword (en)
Aerodynamics Leading edge Experimental study Test facility Speed measurement Flat plate Oscillating aerofoil Moving robot Robotics Vortex Unmanned aerial vehicle Particle image velocimetry
Keyword (es)
Aerodinámica Borde ataque Estudio experimental Instalación ensayo Medida velocidad Placa plana Perfil oscilante Robot móvil Robótica 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

Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D02 Computer science; control theory; systems / 001D02D Control theory. Systems / 001D02D11 Robotics

Discipline
Computer science : theoretical automation and systems Physics : fluid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
27179172

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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