Exploració per autor "Lee, D.S."
Ara es mostren els items 1-5 de 5
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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)
Text en actes de congrés
Accés restringit per política de l'editorialComputational 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)
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Accés obertThis 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)
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Accés restringit per política de l'editorialIn 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'editorialThe 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'editorialThe 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. ...