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Werkstoff
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Active Warping Control of a Joined Wing/Tail Airplane Configuration
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-2001-1210 Aerodynamic Impulse Response of a Panel Method
AIAA-2001-1371 Aeroelastic Response of Multi-Segmented Hinged Wings
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-2004-1654 A Framework for Morphing Capability Assessment
AIAA-2004-1761 Optimum Design Framework for Integrally Twisted Helicopter Blades
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-2004-2038 Reduced Structural Modeling of Integrally-Strained Slender Wings
AIAA-2006-1636 Dynamic Response of Highly Flexible Flying Wings