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Aeroelastic Analysis of Composite Wings
Aeroelastic Control Using Multiple Control Surfaces
Aeroelasticity and Flight Dynamics of Oblique Flying Wings AIAA Paper 2007-2240 CD-ROM Number 7
Aeroelastic Optimization of a Composite Tilt Rotor
Aeroelastic Shape Optimization of a Pluging Plate
Aeroelastic Stability of Composite Hingeless Rotors with Advanced Configurations
Aeroelastic Stability of Composite Rotor Blades in Hover
A Historical Perspective on Rotary Wing Dynamics and Aeroelasticity
A Hybrid Quasi-steady CFD-Inflow Approach for Gust Response Analysis of Highly Flexible Aircraft
AIAA-2001-1204 Optimization of a Composite Pitch-Controlled Variable-Speed Wind Turbine
AIAA-2001-1460 From Fluttering Wings to Flapping Flight: The Energy Connection
AIAA-2001-1530 Validation of the Variational Asymptotic Beam Sectional Analysis (VABS)
AIAA-2001-1535 A Symbolic Methodology for the Stability Analysis of Flexible Rotating Systems
AIAA-2001-1656 Effect of Thrust on Bending-Torsion Flutter of Wings
AIAA-2004-1520 The Vlasov Theory of the Variational Asymptotic Beam Sectional Analysis
AIAA-2004-1650 A Simple Thermopiezoelastic Model for Composite Shells with Accurate Stress Recovery
AIAA-2004-1837 Structural Optimization of Composite Rotor Blades
AIAA-2004-2025 Effect of Configuration Parameters on the Response and Stability of HAWT's
AIAA-2006-1638 Gust Response of Highly Flexible Aircraft
AIAA-2006-1640 Time Domain Nonlinear Aeroelastic Analysis for HALE Wings
AIAA-2006-1656 Modeling of Ground Vibration Testing for Highly Flexible Aircraft
AIAA-2006-1822 Coupling Global and Local Aspects of Cross-Sectional Optimization for Rotor Blades
AIAA-2006-2040 Nonlinear Modeling and Control Design of Active Helicopter Blades
AIAA-2006-2105 Geometrically-Exact, Intrinsic Theory for Dynamics of Moving Composite Plates
Analysis of Beam Contact Problems via Optimal Control Theory
An Evaluation of Computational Algorithms to Interface Between CFD and CSD Methodologies
Applications of an Asymptotic/Modal Approach for Dynamical Modeling of Anisotropic Beams
Asymptotic Beam Theory for Planar Deformation of Initially Curved Isotropic Strips
Asymptotic Construction of a Thermopiezoelastic Model for Smart Composite Plates
Buckling and Crack Propagation of Cracked Box Beams
Composite Beam Cross-Sectional Modeling Including Obliqueness and Trapeze Efects
Cross-Sectional Sizing and Optimization of Composite Blades
Dynamics and Aeroelastic Analysis of Missiles
Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft
End Effects in Thin-Walled Beams
Energy Perspectives in Aeroelastic Control
Enhancement of Roll Maneuverability Using Post-Reversal Design. Part I: Nonlinear Analysis
Finite Element Solution of Nonlinear Intrinsic Equations for Curved Composite Beams
Investigation of the Effect of Damage Shape and Beam Shape Using a Unified Framework
Limit Cycle Oscillations of Aircraft Due to Flutter-Induced Drag
Modeling Beams with Various Boundary Conditions Using Fully Intrinsic Equations
Multi-flexible-body Aeroelastic Analysis of Rotating Systems with Flexible Components
Nonlinear Aeroelastic Analysis of Aircraft with High-aspect-ratio Wings
Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft
Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft with Fully Intrinsic Equations
Nonlinear Aeroelastic Scaling of a Joined Wing Aircraft