Publication | Closed Access
Influence of modelling and solution methods on the FE-simulation of the post-buckling behaviour of stiffened aircraft fuselage panels
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References
2006
Year
EngineeringAerospace EngineeringMechanical EngineeringStructural AnalysisStructural DesignAircraft Fuselage PanelsAerostructureStructural OptimizationComputational MechanicsStructural MechanicsPost-buckling BehaviourAircraft Design ProcessThin-walled StructureSolution MethodsStructural Engineering
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