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Werkstoff
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ZEUS-DO: Design Oriented CFD-Based Unsteady Aerodynamics for Flight Vehicle Shape Optimization
Studies of Aerodynamic Influence of Under-Wing Stores on Flutter Characteristics of F-16
Extension of MSC Nastran UVLM.OpenFSI for Rotational Applications Including Wind Turbines
Behavior of Epoxy Nanocomposites under the Vacuum Ultraviolet Irradiation
A POD-based Reduced Order Design Scheme for Shape Optimization of Air Vehicles
Continuous Dynamic Simulation for Morphing Wing Aeroelasticity
Enabling Sensitivity Analysis Capability for a CFD-Based Unsteady Aerodynamic/Aeroelastic Solver
Dynamic Nonlinear Aeroelastic Analysis of the Joined Wing Configuration
A Multidisciplinary Analysis Optimization Environment for Wings Having SpaRibs
A Multi-Fidelity Multi-Strategy and Multi-Disciplinary Design Optimization Environment
AIAA-2006-1640 Time Domain Nonlinear Aeroelastic Analysis for HALE Wings
AIAA-2006-1851 Flight-Loads Effects on Free-Play Induced Limit Cycle Oscillation
AIAA-2004-1944 Nonlinear Aeroelastic Studies on a Joined-Wing with Wing Buckling Effects
AIAA-2004-1938 Nonlinear Aeroelastic Modeling by Block-Oriented Identification
Limit-Cycle-Oscillation Studies of a Fighter with External Stores
AIAA-2001-1290 Simulation of Transonic Limit Cycle Oscillations Using a CFD Time-Marching Method
Integration of a Steady/Unsteady Wing-body Aerodynamic Module Into ASTROS
Hover Testing of a Smart Rotor With Induced-Strain Actuation of Blade Twist
Unsteady Sonic Aerodynamics Using Acceleration Potential Approach
Nonlinear Response of Open/Closed-Loop Aeroelastic System Using a Discrete State-Space Approach
Body-Flexure Control with Smart Actuation for Hypervelocity Missiles
Extension of the g-Method Flutter Solution to Aeroservoelastic Stability Analysis
Influence of External Store Aerodynamics on Flutter/LCO of a Fighter Aircraft