• 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)
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    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 ...
  • Double Shock Control Bump Design Optimization Using Hybridised Evolutionary Algorithms 

    Lee, DongSeop; Periaux, Jacques; Pons-Prats, Jordi; Bugeda Castelltort, Gabriel; Oñate Ibáñez de Navarra, Eugenio (IEEE Computer Society Publications, 2010)
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    The paper investigates two advanced optimisation methods for solving active flow control device shape design problem and also compares their optimisation efficiency in terms of computational cost and design quality. The ...
  • Lift maximization with uncertainties for the optimization of high-lift devices 

    Zhili, Tang; Periaux, Jacques; Bugeda Castelltort, Gabriel; Oñate Ibáñez de Navarra, Eugenio (2010-09-20)
    Article
    Accés obert
    In this paper, the aerodynamic shape optimization problems with uncertain operating conditions have been addressed. After a review of robust control theory and the possible approaches to take into account uncertainties, ...
  • Multi-objective design optimization of morphing UAV aerofoil/wing using hybridised MOGA 

    Lee, DongSeop; Gonzalez, L F.; Periaux, Jacques; Bugeda Castelltort, Gabriel (2012)
    Comunicació de congrés
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    The paper investigates two advanced Computational Intelligence Systems (CIS) for a morphing Unmanned Aerial Vehicle(UAV) aerofoil/wing shape design optimisation. The first CIS uses Genetic Algorithm (GA) and the second CIS ...
  • 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)
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    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)
    Capítol de llibre
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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)
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    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. ...