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Werkstoff
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Vibrational behavior of adaptive aircraft wing structures modelled as composite thin-walled beams
AIAA-2006-1835 Time-Delayed Feedback Control of a 2-D Supersonic Flapped Wings
AIAA-2006-1739 Dynamics of Thin-Walled Composite Aircraft Wings Carrying External Stores
AIAA-2006-2107 Free Vibration of Doubly-Curved Sandwich Panels with Laminated Face Sheets
AIAA-2006-1731 Aerothermoelastic Stability of Composite Aircraft Wings Subjected to Heat Inputs
AIAA-2006-1872 Modeling, Vibration and Instability of an Advanced Tiltrotor-Wing System
AIAA-2006-1836 Robust Aeroelastic Control of 2-D Supersonic Flapped Lifting Surfaces
AIAA-2004-2046 Aeroelastic Response of Composite Aircraft Swept Wings Impacted by a Laser Beam
AIAA-2004-2049 Thin-Walled Rotating Composite Blades Featuring Extension-Twist Elastic Coupling