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Effect of a centerbody on the vortex flow of a double-delta wing with leading edge extension

Author
MYONG HWAN SOHN1 ; JO WON CHANG2
[1] Department of Mechanical Engineering, Pohang University of Science and Technology, Gyeongbuk 790-784, Korea, Republic of
[2] Department of Aeronautical Science and Flight Operation, Korea Aerospace University, Gyeonggi 412-791, Korea, Republic of
Source

Aerospace science and technology (Imprimé). 2010, Vol 14, Num 1, pp 11-18, 8 p ; ref : 12 ref

ISSN
1270-9638
Scientific domain
Aeronautics astronautics; Mechanics acoustics
Publisher
Elsevier, Issy-les-Moulineaux
Publication country
France
Document type
Article
Language
English
Author keyword
Centerbody Double-delta wing Off-surface flow visualization Vortex flow Wing-surface pressure measurement
Keyword (fr)
Aile delta Aérodynamique Bord attaque Ecoulement tourbillonnaire Essai sur modèle Etude expérimentale Forme géométrique Mesure pression Visualisation écoulement 4785G
Keyword (en)
Delta wing Aerodynamics Leading edge Vortex flow Model test Experimental study Geometrical shape Pressure measurement Flow visualization
Keyword (es)
Ala delta Borde ataque Ensayo sobre modelo Forma geométrica
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
22296123

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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