Minimum weight design of curvilinearly grid-stiffened variable-stiffness composite fuselage panels considering buckling and manufacturing constraints
Ahmad Alhajahmad, Christian Mittelstedt
Topics & Concepts
FuselageBucklingStructural engineeringEngineeringStiffnessGridMinimum weightComposite numberCurvilinear coordinatesMaterials scienceMathematicsComposite materialGeometryComposite Structure Analysis and OptimizationTopology Optimization in EngineeringStructural Analysis and Optimization