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Werkstoff
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Aeroelastic Characteristic of an Airfoil Containing Laminated Composite Plate (AIAA 2014-1196)
Validation of an UAV F.E. Model Using Operational Data (AIAA 2014-0333)
Post-Flutter Analysis of Flexible High-Aspect-Ratio Wings
Progressive Failure Analysis of Wind Turbine Blades Based on a Thin-Wall Beam Finite Element Model
Dynamic Identification of Wind Turbine System Under Operational Conditions Using FBG Transducers
Durability of Tapered Composite Laminates under Static and Fatigue Loading
Modeling of Geometrically Nonlinear Aeroelasticity of Advanced Aircraft Wings in Incompressible Flow
Modal Interactions in a Geometrically Nonlinear Cantilevered Beam
Nonlinear Aero-Thermo-Visco-Elastic Behavior of Geometrically Imperfect Curved Skin Panel
Nonlinear Dynamical Modeling of a High Altitude Long Endurance Unmanned Aerial Vehicle
AIAA-2006-2110 Localized Magnetoelastic Bending Vibration of an Electroconductive Elastic Plate
AIAA-2006-1835 Time-Delayed Feedback Control of a 2-D Supersonic Flapped Wings
AIAA-2006-1823 Design and Shape Optimization of Inflatable Wings
AIAA-2006-2186 Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings
AIAA-2006-2161 Aeroelastic Behavior of a Non-Rigidizable Inflatable UAV Wing
AIAA-2006-1836 Robust Aeroelastic Control of 2-D Supersonic Flapped Lifting Surfaces
AIAA-2006-1641 Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs
AIAA-2006-1701 Static, Buckling and Dynamic Behavior of Inflatable Beams
AIAA-2004-1673 Aeroelastic Response of Flapped Wing Systems Using Robust Estimation Methodology
2003-01-0576 A Study on the Bending Springback of Aluminum Alloy 5754
Active Aeroelastic Control of 2-D Wing-Flap Systems in an Incompressible Flowfield
Circular Cylindrical Shells Immersed in a Magnetic Field: Modeling and Dynamic Behavior
Nonlinear Time Delayed Feedback Control of Aeroelastic Systems: A Functional Approach
Analysis of a 2-D Supersonic Lifting Surface with Time Delayed Feedback Control
Open/Closed-Loop Nonlinear Aeroelasticity for Airfoils via Volterra Series Approach
Static/Dynamic Solutions and Validation of a Refined Anisotropic Thin-Walled Beam Model
AIAA-2001-1459 Volterra Series Approach for Nonlinear Aeroelastic Response of 2-D Lifting Surfaces