Browsing by Author "Lee, D.S."

Now showing items 1-5 of 5

    • Advanced computational intelligence system for inverse aeronautical design optimisation 

      Lee, D.S.; Periaux, Jacques; Oñate Ibáñez de Navarra, Eugenio; Gonzalez, L. (Institute of Electrical and Electronics Engineers (IEEE), 2011)
      Conference report
      Restricted access - publisher's policy
      Computational Intelligence Systems (CIS) is one of advanced softwares. CIS has been important position for solving single-objective / reverse / inverse and multi-objective design problems in engineering. The paper hybridise ...

    • Green design and multidisciplinary optimization of carbon nanotube composite structures 

      Morillo, Carlos; Bugeda Castelltort, Gabriel; Lee, D.S.; Oller Martínez, Sergio Horacio (Universidad de las Palmas de Gran Canaria, 2013)
      Conference report
      Open Access
      This work develops a multi-objective design optimisation method for Carbon Nanotube Composite Structures (CNTCSs) using Genetic Algorithm and Finite Element Analysis (FEA). Two design problems are considered: the first is ...

    • Robust aerodynamic design optimisation of morphing aerofoil/wing using distributed MOGA 

      Lee, D.S.; Gonzalez, L.F.; Periaux, Jacques; Oñate Ibáñez de Navarra, Eugenio (International Council of the Aeronautical Sciences (ICAS), 2012)
      Conference report
      Restricted access - publisher's policy
      In this paper, the shape design optimisation using morphing aerofoil/wing techniques, namely the leading and/or trailing edge deformation of a natural laminar flow RAE 5243 aerofoil is investigated to reduce transonic ...

    • Shock control bump design optimization on natural laminar aerofoil 

      Lee, D.S.; Periaux, Jacques; Srinivas, K.; Gonzalez, L.F.; Qin, N.; Oñate Ibáñez de Navarra, Eugenio (Springer-Verlag, 2011)
      Part of book or chapter of book
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      The paper investigates Shock Control Bumps (SCB) on a Natural Laminar Flow (NLF) aerofoil; RAE 5243 for Active Flow Control (AFC). A SCB approach is used to decelerate supersonic flow on the suction/pressure sides of ...

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

      Lee, D.S.; Srinivas, K.; Periaux, Jacques; Oñate Ibáñez de Navarra, Eugenio (2012)
      Conference report
      Restricted access - publisher's policy
      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. ...