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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DOI
10.2514/1.34112 
https://dx.doi.org/10.2514/1.34112
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