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Werkstoff
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The Timoshenko-like Theory of the Variational Asymptotic Beam Sectional Analysis
Theory of Initially Twisted, Composite, Thin-walled Beams
Stiffness Constants for Composite Beams Including Large Initial Twist and Curvature Effects
Stability Analysis of Columns with Imperfection
Rigorous Joining of Advanced Reduced-Dimensional Beam Models to 2-D Finite Element Models
Parametric Study of Joined-Wing Aircraft Geometry
On Static Stability of Damaged Columns
On Asymptotically Correct Plate Theory
Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft with Fully Intrinsic Equations
Nonlinear Aeroelastic Analysis of Aircraft with High-aspect-ratio Wings
Multi-flexible-body Aeroelastic Analysis of Rotating Systems with Flexible Components
Modeling Beams with Various Boundary Conditions Using Fully Intrinsic Equations
Investigation of the Effect of Damage Shape and Beam Shape Using a Unified Framework
Finite Element Solution of Nonlinear Intrinsic Equations for Curved Composite Beams
Enhancement of Roll Maneuverability Using Post-Reversal Design. Part I: Nonlinear Analysis
End Effects in Thin-Walled Beams
Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft
Dynamics and Aeroelastic Analysis of Missiles
Cross-Sectional Sizing and Optimization of Composite Blades
Composite Beam Cross-Sectional Modeling Including Obliqueness and Trapeze Efects
Asymptotic Construction of a Thermopiezoelastic Model for Smart Composite Plates
Asymptotic Beam Theory for Planar Deformation of Initially Curved Isotropic Strips
Applications of an Asymptotic/Modal Approach for Dynamical Modeling of Anisotropic Beams
An Evaluation of Computational Algorithms to Interface Between CFD and CSD Methodologies
Analysis of Beam Contact Problems via Optimal Control Theory
AIAA-2006-2105 Geometrically-Exact, Intrinsic Theory for Dynamics of Moving Composite Plates
AIAA-2006-1822 Coupling Global and Local Aspects of Cross-Sectional Optimization for Rotor Blades
AIAA-2006-1656 Modeling of Ground Vibration Testing for Highly Flexible Aircraft
AIAA-2004-2025 Effect of Configuration Parameters on the Response and Stability of HAWT's
AIAA-2004-1837 Structural Optimization of Composite Rotor Blades
AIAA-2004-1650 A Simple Thermopiezoelastic Model for Composite Shells with Accurate Stress Recovery
AIAA-2004-1520 The Vlasov Theory of the Variational Asymptotic Beam Sectional Analysis
AIAA-2001-1656 Effect of Thrust on Bending-Torsion Flutter of Wings
AIAA-2001-1535 A Symbolic Methodology for the Stability Analysis of Flexible Rotating Systems
AIAA-2001-1530 Validation of the Variational Asymptotic Beam Sectional Analysis (VABS)
AIAA-2001-1204 Optimization of a Composite Pitch-Controlled Variable-Speed Wind Turbine
A Historical Perspective on Rotary Wing Dynamics and Aeroelasticity
Aeroelastic Stability of Composite Rotor Blades in Hover
Aeroelastic Stability of Composite Hingeless Rotors with Advanced Configurations
Aeroelastic Optimization of a Composite Tilt Rotor
Aeroelastic Analysis of Composite Wings