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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
Dynamics of Pretwisted Rotating Thin-walled Beams Operating in a Temperature Field
Enhancement of the Thermomechanical Load Carrying Capacity of Advanced Sandwich Structures
Dynamic Response of Adaptive Cantilevers with External Stores Subjected to Blast Loading
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
A Comprehensive Nonlinear Model for Sandwich-Shells with Anisotropic Faces and Compressible Core
Electromagnetically Conducting Elastic Plates in a Magnetic Field: Modeling and Dynamic Implications
Vibration of Pretwisted Shearable Rotating Composite Beams
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
Nonlinear Time Delayed Feedback Control of Aeroelastic Systems: A Functional Approach
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
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-2006-2110 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