Effect of Gurney flap on unsteady wake vortex
- Author
- LEE, L1 ; LEE, T1
[1] McGill University, Montreal, Quebec, H3A 2K6, Canada - Source
Journal of aircraft. 2007, Vol 44, Num 4, pp 1398-1401, 4 p ; ref : 9 ref
- CODEN
- JAIRAM
- ISSN
- 0021-8669
- Scientific domain
- Aeronautics astronautics; Mechanical engineering; Mechanics acoustics; Transportation
- Publisher
- American Institute of Aeronautics and Astronautics, Reston, VA
- Publication country
- United States
- Document type
- Article
- Language
- English
- Keyword (fr)
- Aile Appareillage Aérodynamique Bord fuite Ecoulement tourbillonnaire Etude expérimentale Portance Profil oscillant Volet 4785G
- Keyword (en)
- Wing Instrumentation Aerodynamics Trailing edge Vortex flow Experimental study Lift Oscillating aerofoil Flap
- Keyword (es)
- Ala Borde salida Perfil oscilante Flap
- 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
- 18992535
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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DOI
10.2514/1.29555 
https://dx.doi.org/10.2514/1.29555
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