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Werkstoff
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Vibrational behavior of adaptive aircraft wing structures modelled as composite thin-walled beams
Effect of Elastic Couplings on Dynamics and Instability of Anisotropic Spinning Thin-Walled Beams
Implications of External Stores on Static and Dynamic Aeroelasticity of Advanced Aircraft Wings
Dynamic Response of Adaptive Cantilevers with External Stores Subjected to Blast Loading
Dynamics of Pretwisted Rotating Thin-walled Beams Operating in a Temperature Field
Enhancement of the Thermomechanical Load Carrying Capacity of Advanced Sandwich Structures
Bending Vibration of Gyroelastic Thin-walled Beams Incorporating Adaptive Capabilities
AIAA-2001-1459 Volterra Series Approach for Nonlinear Aeroelastic Response of 2-D Lifting Surfaces
Vibration of Pretwisted Shearable Rotating Composite Beams
Electromagnetically Conducting Elastic Plates in a Magnetic Field: Modeling and Dynamic Implications
A Comprehensive Nonlinear Model for Sandwich-Shells with Anisotropic Faces and Compressible Core
Comparative Study on Vibration Control Methodologies Applied to Adaptive Anisotropic Cantilevers
Open/Closed-Loop Nonlinear Aeroelasticity for Airfoils via Volterra Series Approach
Static/Dynamic Solutions and Validation of a Refined Anisotropic Thin-Walled Beam Model
Thermally Induced Bending Vibration of Composite Spacecraft Booms Subjected to Solar Heating
2003-01-0576 A Study on the Bending Springback of Aluminum Alloy 5754
Core and Face Sheet Anisotropy in Deformation and Buckling of Sandwich Panels
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
Analysis of a 2-D Supersonic Lifting Surface with Time Delayed Feedback Control
Thin-Walled Rotating Blades made of Functionally Graded Materials: Modeling and Vibration Analysis
Nonlinear Vibration of Finitely Electroconductive Plate-Strips in a Magnetic Field
Optimal Control of Pretwisted Shearable Smart Composite Rotor Blades
Nonlinear Time Delayed Feedback Control of Aeroelastic Systems: A Functional Approach
Modeling the Structural Response of Multifunctional Materials: The In-field Vibration of Thin Plates
AIAA-2004-2046 Aeroelastic Response of Composite Aircraft Swept Wings Impacted by a Laser Beam
AIAA-2004-1673 Aeroelastic Response of Flapped Wing Systems Using Robust Estimation Methodology
AIAA-2004-2049 Thin-Walled Rotating Composite Blades Featuring Extension-Twist Elastic Coupling
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-2006-1739 Dynamics of Thin-Walled Composite Aircraft Wings Carrying External Stores
AIAA-2006-1835 Time-Delayed Feedback Control of a 2-D Supersonic Flapped Wings