Synonyme wurden verwendet für:
Werkstoff
Suche ohne Synonyme:
keywords:(Werkstoff)
Aeroelastic Characteristic of an Airfoil Containing Laminated Composite Plate (AIAA 2014-1196)
Validation of an UAV F.E. Model Using Operational Data (AIAA 2014-0333)
Post-Flutter Analysis of Flexible High-Aspect-Ratio Wings
Nonlinear Aero-Thermo-Visco-Elastic Behavior of Geometrically Imperfect Curved Skin Panel
Dynamic Identification of Wind Turbine System Under Operational Conditions Using FBG Transducers
Nonlinear Dynamical Modeling of a High Altitude Long Endurance Unmanned Aerial Vehicle
Modal Interactions in a Geometrically Nonlinear Cantilevered Beam
Progressive Failure Analysis of Wind Turbine Blades Based on a Thin-Wall Beam Finite Element Model
Durability of Tapered Composite Laminates under Static and Fatigue Loading
Modeling of Geometrically Nonlinear Aeroelasticity of Advanced Aircraft Wings in Incompressible Flow
Vibrational behavior of adaptive aircraft wing structures modelled as composite thin-walled beams
AIAA-2006-1701 Static, Buckling and Dynamic Behavior of Inflatable Beams
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-2006-1739 Dynamics of Thin-Walled Composite Aircraft Wings Carrying External Stores
AIAA-2006-1823 Design and Shape Optimization of Inflatable Wings
AIAA-2006-2186 Nonlinear Aeroelastic Modeling and Experiments of Flexible Wings
AIAA-2006-1872 Modeling, Vibration and Instability of an Advanced Tiltrotor-Wing System
AIAA-2006-2161 Aeroelastic Behavior of a Non-Rigidizable Inflatable UAV Wing
AIAA-2006-1836 Robust Aeroelastic Control of 2-D Supersonic Flapped Lifting Surfaces
AIAA-2006-1641 Stability, Control, and Simulation of High-Altitude-Long-Endurance UAVs
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-2004-2049 Thin-Walled Rotating Composite Blades Featuring Extension-Twist Elastic Coupling
AIAA-2004-1673 Aeroelastic Response of Flapped Wing Systems Using Robust Estimation Methodology
AIAA-2004-2046 Aeroelastic Response of Composite Aircraft Swept Wings Impacted by a Laser Beam
2003-01-0576 A Study on the Bending Springback of Aluminum Alloy 5754