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Werkstoff
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keywords:(Werkstoff)
Parametric Study of Joined-Wing Aircraft Geometry
Enhancement of Roll Maneuverability Using Post-Reversal Design. Part I: Nonlinear Analysis
Modeling Beams with Various Boundary Conditions Using Fully Intrinsic Equations
Random Crack Propagation Analysis of a Beam with a Crack
A Hybrid Quasi-steady CFD-Inflow Approach for Gust Response Analysis of Highly Flexible Aircraft
Nonlinear Aeroelastic Scaling of a Joined Wing Aircraft
On Static Stability of Damaged Columns
Aeroelastic Shape Optimization of a Pluging Plate
Stability and Power Optimality in Time-Periodic Flapping Wing Structures
Rigorous Joining of Advanced Reduced-Dimensional Beam Models to 2-D Finite Element Models
Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft
Buckling and Crack Propagation of Cracked Box Beams
Stability Analysis of Columns with Imperfection
Asymptotic Beam Theory for Planar Deformation of Initially Curved Isotropic Strips
Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations
Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft with Fully Intrinsic Equations
Parametric Representation and Shape Optimization of a Wing for Flapping Micro Air Vehicles
Investigation of the Effect of Damage Shape and Beam Shape Using a Unified Framework