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