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Aerodynamic Redesign Using Discrete Adjoint Approach on Overset Mesh System

Author
BYUNG JOON LEE1 ; KIM, Chongam1
[1] Seoul National University, Seoul 151-744, Korea, Republic of
Source

Journal of aircraft. 2008, Vol 45, Num 5, pp 1643-1653, 11 p ; ref : 25 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)
Avion Aérodynamique Aéronef Conception optimale Forme géométrique Génération maille Modélisation Méthode adjoint Optimisation Simulation numérique
Keyword (en)
Airplane Aerodynamics Aircraft Optimal design Geometrical shape Mesh generation Modeling Adjoint method Optimization Numerical simulation
Keyword (es)
Avión Aerodinámica Aeronave Concepción optimal Forma geométrica Modelización Método adjunto Optimización Simulación numérica
Classification
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
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
20778521

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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