• 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. ...