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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
Dynamic Identification of Wind Turbine System Under Operational Conditions Using FBG Transducers
Progressive Failure Analysis of Wind Turbine Blades Based on a Thin-Wall Beam Finite Element Model
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-2006-1823 Design and Shape Optimization of Inflatable 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-2006-2186 Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings
AIAA-2006-1701 Static, Buckling and Dynamic Behavior of Inflatable Beams
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-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
Analysis of a 2-D Supersonic Lifting Surface with Time Delayed Feedback Control
Circular Cylindrical Shells Immersed in a Magnetic Field: Modeling and Dynamic Behavior
Nonlinear Time Delayed Feedback Control of Aeroelastic Systems: A Functional Approach
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