Carregant...
Carregant...

Vés al contingut (premeu Retorn)

Shock-free aerofoil/wing design optimisation via morphing technique: leading and trailing edge deformation

Autor
Srinivas; Périaux, J.; Lee, D.S.; Oñate, E.
Tipus d'activitat
Presentació treball a congrés
Nom de l'edició
7th International Conference on Computational Fluid Dynamics
Any de l'edició
2012
Data de presentació
2012-07
Llibre d'actes
7th International Conference on Computational Fluid Dynamics
Pàgina inicial
1
Pàgina final
10
Repositori
http://hdl.handle.net/2117/19121 Obrir en finestra nova
URL
http://www.iccfd.org/iccfd7/assets/pdf/abstracts/ICCFD7-2404_abstract.pdf Obrir en finestra nova
Resum
Morphing Aerofoil/Wing, Computational Fluid Dynamics, Evolutionary Algorithms, Shock-Free Aerofoil/Wing The paper investigates the drag reduction of aerofoils and wings using a morphing technique which consists of deforming the leading and trailing edges. It is treated as an optimisation procedure using Evolutionary Algorithms. For the purpose, an in house code - Multi-Objective Genetic Algorithm (MOGA) under High Performance Computing (HPC) environment is used. An Euler code with viscous correc...
Citació
Lee, D.S. [et al.]. Shock-free aerofoil/wing design optimisation via morphing technique: leading and trailing edge deformation. A: International Conference on Computational Fluid Dynamics. "7th International Conference on Computational Fluid Dynamics". 2012, p. 1-10.
Grup de recerca
(MC)2 - UPC Mecànica de Medis Continus i Computacional
GMNE - Grup de Mètodes Numèrics en Enginyeria

Participants