Generalized Unified Formulation Shell Element for Functionally Graded Variable-Stiffness Composite Laminates and Aeroelastic Applications
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
2015-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2015
|Static Aeroelastic Optimization of Composite Wings with Variable Stiffness Laminates
German Aerospace Center (DLR) | 2014
|