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Werkstoff
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keywords:(Werkstoff)
Aeroelastic Analysis of Composite Wings
Aeroelastic Optimization of a Composite Tilt Rotor
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
AIAA-2001-1204 Optimization of a Composite Pitch-Controlled Variable-Speed Wind Turbine
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-2006-1656 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-2006-2105 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
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
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
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 with Fully Intrinsic Equations
On Asymptotically Correct Plate Theory
On Static Stability of Damaged Columns
Parametric Study of Joined-Wing Aircraft Geometry
Rigorous Joining of Advanced Reduced-Dimensional Beam Models to 2-D Finite Element Models
Stability Analysis of Columns with Imperfection
Stiffness Constants for Composite Beams Including Large Initial Twist and Curvature Effects
Theory of Initially Twisted, Composite, Thin-walled Beams
The Timoshenko-like Theory of the Variational Asymptotic Beam Sectional Analysis