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Werkstoff
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Parametric Study of Joined-Wing Aircraft Geometry
Optimum Designer/Tailored Stitched Composites
Enhancement of Roll Maneuverability Using Post-Reversal Design. Part I: Nonlinear Analysis
Modeling Beams with Various Boundary Conditions Using Fully Intrinsic Equations
Optimum Stress and Material Distributions in Stitched PRSEUS Composites
Studies of Aerodynamic Influence of Under-Wing Stores on Flutter Characteristics of F-16
Stability Analysis of Columns with Imperfection
Assessment of Impact of Modeling Simplifications for a Medium Voltage DC Shipboard Power System
Rigorous Joining of Advanced Reduced-Dimensional Beam Models to 2-D Finite Element Models
On Static Stability of Damaged Columns
Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft
Asymptotic Beam Theory for Planar Deformation of Initially Curved Isotropic Strips
Optimum Designer Materials and Geometries for Stitched PRSEUS Composites
Negative Stress Margins - Are They Real?
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
A Multi-Fidelity Multi-Strategy and Multi-Disciplinary Design Optimization Environment