A Comprehensive Nonlinear Model for Sandwich-Shells with Anisotropic Faces and Compressible Core
Active Aeroelastic Control of 2-D Wing-Flap Systems in an Incompressible Flowfield
Active Vibration Control of Composite Spacecraft Booms Exposed To Solar Radiant Heating
A dynamic nonlinear model of multilayered composite shells featuring damaged interfaces
Aerodynamic indicial functions and their use in aeroelastic formulation of lifting surfaces
Aeroelastic Response and Active Control of Aircraft Wings Modeled as Thin-Walled Beams
Aeroelastic Response and Active Control of an Airfoil in a Subsonic Compressible Flow
Aeroelastic Response of Composite Aircraft Swept Wings Impacted by a Laser Beam
Aeroelastic Response of Flapped Wing Systems Using Robust Estimation Methodology
Aerothermoelastic Stability of Composite Aircraft Wings Subjected to Heat Inputs
Analysis of a 2-D Supersonic Lifting Surface with Time Delayed Feedback Control
Bending vibration of gyroelastic thin-walled beams incorporating adaptive capabilities
Circular Cylindrical Shells Immersed in a Magnetic Field: Modeling and Dynamic Behavior
Comparative Study on Vibration Control Methodologies Applied to Adaptive Anisotropic Cantilevers
Core and Face Sheet Anisotropy in Deformation and Buckling of Sandwich Panels
Dynamic response of adaptive cantilevers with external stores subjected to blast loading
Dynamics and Instability of Current-Carrying Cylindrical Shells in a Magnetic Field
Dynamics of pretwisted rotating thin-walled beams operating in a temperature field