Exploració per autor "Periaux, Jacques"

Ara es mostren els items 3-7 de 7

    • 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)
      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
      Accés restringit per política de l'editorial
      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)
      Text en actes de congrés
      Accés restringit per política de l'editorial
      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
      Accés restringit per política de l'editorial
      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)
      Text en actes de congrés
      Accés restringit per política de l'editorial
      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. ...