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Compliant assembly variation analysis of aeronautical panels using unified substructures with consideration of identical parts

EngineeringAerospace EngineeringAeronautical PanelsMechanical EngineeringDesignStructural TopologyIdentical PartsStructural DesignAssembly LineComputer-aided DesignStructural OptimizationComputational MechanicsStructural MechanicsAircraft Design ProcessAerostructureUnified Substructures