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Multidisciplinary Design Optimization of an UAV Wing Using Kriging Based Multi-Objective Genetic Algorithm
2009
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
unpublished
This paper investigates the preliminary wing design of Unmanned Aerial Vehicle (UAV) using a two step optimization approach. The first step is a single objective aerodynamic optimization whereas the second step is a coupled dual objective aerodynamic and structural optimization. In the single objective case, airfoil geometry is optimized to get maximum endurance parameter at a 2D level with maximum thickness to chord ratio and maximum camber as design variables. Constraints are imposed on the
doi:10.2514/6.2009-2219
fatcat:yzyls34fqzb73mmmpyvioxhsle