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Performance Enhancement of a Vertical Tail Using Synthetic Jet Actuators

Author
RATHAY, Nicholas W1 ; BOUCHER, Matthew J1 ; AMITAY, Michael1 ; WHALEN, Edward2
[1] Rensselaer Polytechnic Institute, Troy, New York 12180, United States
[2] The Boeing Company, Hazelwood, Missouri 36042, United States
Conference name
Aerospace Sciences Meeting (50 ; Nashville, TN 2012-01-09)
Source

AIAA journal. 2014, Vol 52, Num 4, pp 810-820, 11 p ; ref : 26 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
Conference Paper
Language
English
Keyword (fr)
Actionneur Avion Aéronef Commande écoulement Configuration géométrique Essai soufflerie Etude expérimentale Installation essai Mesure pression Queue Stéréoscopie Vélocimétrie image particule 4762
Keyword (en)
Actuator Airplane Aircraft Flow control Geometrical configuration Wind tunnel test Experimental study Test facility Pressure measurement Tail Stereoscopy Particle image velocimetry
Keyword (es)
Accionador Avión Aeronave Configuración geométrica Ensayo túnel aerodinámico Estudio experimental Instalación ensayo Medida presión Cola Estereoscopia
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 / 001D Applied sciences / 001D15 Ground, air and sea transportation, marine construction / 001D15I Air transportation and traffic

Discipline
Building. Public works. Transport. Civil engineering Physics : fluid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
28415763

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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