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Design of variable-stiffness composite panels for maximum buckling load

Journal article (2009) - S Setoodeh, M.M. Abdalla, S.T. IJsselmuiden, Z. Gurdal

Design of Variable-Stiffness Conical Shells for Maximum Fundamental Eigenfrequency

Journal article (2008) - AW Blom, S Setoodeh, J.M.A.M. Hol, Z. Gurdal

Design of Variables Stiffness Panels for Maximum Buckling Load Using Lamination Parameters

Conference paper (2008) - S.T. IJsselmuiden, M.M. Abdalla, S Setoodeh, Z. Gurdal

Design of variable stiffness composite panels for maximum fundamental frequency using lamination parameters

Journal article (2007) - M.M. Abdalla, S Setoodeh, Z. Gurdal

Design of Variable-Stiffness Conical Shells for Maximum Fundamental Frequency

Conference paper (2006) - AW Blom, S Setoodeh, J.M.A.M. Hol, Z. Gurdal

Approximate Feasible Regions for Lamination Parameters

Conference paper (2006) - S Setoodeh, M.M. Abdalla, Z. Gurdal

Design of variable-stiffness composite layers using cellular automata

Journal article (2006) - S Setoodeh, Z. Gurdal, LT Watson

Generating Curvilinear Fiber Paths from Lamination Parameters Distribution

Conference paper (2006) - S Setoodeh, AW Blom

Pipeline Implementation of Cellular Automata for Structural Design on Message-passing Multiprocessors

Journal article (2006) - S Setoodeh, DB Adams, Z. Gurdal, LT Watson

Design of Variable-Stiffness Composite Panels for Maximum Buckling Load

Conference paper (2006) - M.M. Abdalla, S Setoodeh, Z. Gurdal

Design of variable-stiffness laminates using lamination parameters

Journal article (2006) - S Setoodeh, M.M. Abdalla, Z. Gurdal

The Cellular Automata Paradigm for Topology Optimisation

Conference paper (2005) - M.M. Abdalla, S Setoodeh, Z. Gurdal

Optimum Design of Variable Stiffness Composites Using Cellular Automata

Doctoral thesis (2005) - S Setoodeh

Design of Variable Stiffness Composite Panels for Maximum Fundamental Frequency Using Lamination Parameters

Conference paper (2005) - S Setoodeh, M.M. Abdalla, Z. Gurdal

Design of Variable Stiffness Laminates for In-Plane Loading Using Lamination Parameters