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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
Random Crack Propagation Analysis of a Beam with a Crack
Modeling Beams with Various Boundary Conditions Using Fully Intrinsic Equations
Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft
A Hybrid Quasi-steady CFD-Inflow Approach for Gust Response Analysis of Highly Flexible Aircraft
Toward an Unsteady Aerodynamic ROM for Multiple Mach Regimes
Nonlinear Aeroelastic Scaling of a Joined Wing Aircraft
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
Buckling and Crack Propagation of Cracked Box Beams
Stability Analysis of Columns with Imperfection
A Multidisciplinary Design Environment for Composite Rotor Blades
Strain-Based Analysis for Geometrically Nonlinear Beams: A Modal Approach