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Werkstoff
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keywords:(Werkstoff)
Modeling of Geometrically Nonlinear Aeroelasticity of Advanced Aircraft Wings in Incompressible Flow
Modal Interactions in a Geometrically Nonlinear Cantilevered Beam
Vibrational behavior of adaptive aircraft wing structures modelled as composite thin-walled beams
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
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
2003-01-0576 A Study on the Bending Springback of Aluminum Alloy 5754
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
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
Active Aeroelastic Control of 2-D Wing-Flap Systems in an Incompressible Flowfield
Core and Face Sheet Anisotropy in Deformation and Buckling of Sandwich Panels
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
Electromagnetically Conducting Elastic Plates in a Magnetic Field: Modeling and Dynamic Implications
Vibration of Pretwisted Shearable Rotating Composite Beams