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title: 31st Structures, Structural Dynamics and Materials Conference
A Refined Structural Dynamics Model for Composite Rotor Blades
AIAA-2006-1663 Dynamics of Insect-Based Flapping Wings: Loads Validation
Structural Modeling of Beams with Skewed Piezoactuators
Aeroelastic Modeling of Trailing-edge Flaps with Smart Material Actuators
Hover Testing of an Active Rotor Blade Tip and Structural Analysis of the Actuator Beam
Active Control of Performance and Vibratory Loads Using Leading Edge Slats
Prediction and Validation of UTTAS Pull-up Maneuver Using CFD/CSD Coupling
Design and Testing of a Quad Shrouded Rotor Micro Air Vehicle in Hover
Towards a Fundamental Understanding of Low Reynolds Number Hover-Capable Flapping Wing Aerodynamics
Aeroelastic Analysis of a MAV-Scale Cycloidal Rotor
Helicopter vibration reduction with trailing edge flaps
Helicopter Vibration Reduction with Trailing Edge Flaps
Hover Testing of a Smart Rotor With Induced-Strain Actuation of Blade Twist
Hover testing of a smart rotor with induced-strain actuation of blade twist
Aeroelastic Analysis of Advanced Geometry Tiltrotor Aircraft
Aeroelastic analysis of advanced geometry tiltrotor aircraft
Formulation of a rotor-system damage detection methodology
Formulation of a Rotor-System Damage Detection Methodology
AIAA-2001-1675 Aeroelastic Stability of Smart Trailing-Edge Flap Helicopter Rotors
AIAA-2001-1358 Open-Loop Hover and Wind Tunnel Testing of Mach-Scaled Rotor with Trailing-Edge Flaps
A Comprehensive Analysis for Whirl Flutter Stability of Two-Bladed Proprotor/Pylon Systems