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Werkstoff
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Parametric Study of Joined-Wing Aircraft Geometry
Enhancement of Roll Maneuverability Using Post-Reversal Design. Part I: Nonlinear Analysis
Implicit LES Simulations of a Flexible Flapping Wing
Modeling Beams with Various Boundary Conditions Using Fully Intrinsic Equations
Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft
Toward an Unsteady Aerodynamic ROM for Multiple Mach Regimes
Stability Analysis of Columns with Imperfection
A Multidisciplinary Design Environment for Composite Rotor Blades
Strain-Based Analysis for Geometrically Nonlinear Beams: A Modal Approach
Simulation of Guided Wave Propagation in Isotropic and Composite Structures using LISA
X-HALE: A Very Flexible UAV for Nonlinear Aeroelastic Tests
Rigorous Joining of Advanced Reduced-Dimensional Beam Models to 2-D Finite Element Models
Structural Models for Flight Dynamic Analysis of Very Flexible Aircraft
On Static Stability of Damaged Columns
Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft
Nonlinear Aeroelastic Framework Based on Vortex-Lattice Method and Corotational Shell Finite Element