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

Author
Srinivas; Périaux, J.; Lee, D.S.; Oñate, E.
Type of activity
Presentation of work at congresses
Name of edition
7th International Conference on Computational Fluid Dynamics
Date of publication
2012
Presentation's date
2012-07
Book of congress proceedings
7th International Conference on Computational Fluid Dynamics
First page
1
Last page
10
Repository
http://hdl.handle.net/2117/19121 Open in new window
URL
http://www.iccfd.org/iccfd7/assets/pdf/abstracts/ICCFD7-2404_abstract.pdf Open in new window
Abstract
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...
Citation
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.
Group of research
(MC)2 - UPC Computational continuum mechanics
GMNE - Numerical Methods in Engineering Group

Participants

  • Srinivas, K.  (author and speaker )
  • Periaux, Jacques Francis  (author and speaker )
  • Lee, Dong Seop  (author and speaker )
  • Oñate Ibáñez de Navarra, Eugenio  (author and speaker )