Synonyme wurden verwendet für:
Werkstoff
Suche ohne Synonyme:
keywords:(Werkstoff)
Vibrational behavior of adaptive aircraft wing structures modelled as composite thin-walled beams
Validation of an UAV F.E. Model Using Operational Data (AIAA 2014-0333)
Thin-Walled Rotating Blades made of Functionally Graded Materials: Modeling and Vibration Analysis
Thermally Induced Bending Vibration of Composite Spacecraft Booms Subjected to Solar Heating
Static/Dynamic Solutions and Validation of a Refined Anisotropic Thin-Walled Beam Model
Progressive Failure Analysis of Wind Turbine Blades Based on a Thin-Wall Beam Finite Element Model
Post-Flutter Analysis of Flexible High-Aspect-Ratio Wings
Open/Closed-Loop Nonlinear Aeroelasticity for Airfoils via Volterra Series Approach
Nonlinear Time Delayed Feedback Control of Aeroelastic Systems: A Functional Approach
Nonlinear Dynamical Modeling of a High Altitude Long Endurance Unmanned Aerial Vehicle
Nonlinear Aero-Thermo-Visco-Elastic Behavior of Geometrically Imperfect Curved Skin Panel
Modeling of Geometrically Nonlinear Aeroelasticity of Advanced Aircraft Wings in Incompressible Flow
Modal Interactions in a Geometrically Nonlinear Cantilevered Beam
Effect of Elastic Couplings on Dynamics and Instability of Anisotropic Spinning Thin-Walled Beams
Dynamics of Pretwisted Rotating Thin-walled Beams Operating in a Temperature Field
Dynamic Identification of Wind Turbine System Under Operational Conditions Using FBG Transducers
Durability of Tapered Composite Laminates under Static and Fatigue Loading
Circular Cylindrical Shells Immersed in a Magnetic Field: Modeling and Dynamic Behavior
Bending Vibration of Gyroelastic Thin-walled Beams Incorporating Adaptive Capabilities
Analysis of a 2-D Supersonic Lifting Surface with Time Delayed Feedback Control
AIAA-2006-2186 Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings
AIAA-2006-2161 Aeroelastic Behavior of a Non-Rigidizable Inflatable UAV Wing
AIAA-2006-2110 Localized Magnetoelastic Bending Vibration of an Electroconductive Elastic Plate
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-2006-1835 Time-Delayed Feedback Control of a 2-D Supersonic Flapped Wings
AIAA-2006-1823 Design and Shape Optimization of Inflatable Wings
AIAA-2006-1739 Dynamics of Thin-Walled Composite Aircraft Wings Carrying External Stores
AIAA-2006-1701 Static, Buckling and Dynamic Behavior of Inflatable Beams
AIAA-2006-1641 Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs
AIAA-2004-2049 Thin-Walled Rotating Composite Blades Featuring Extension-Twist Elastic Coupling