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Werkstoff
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Enhancement of Roll Maneuverability Using Post-Reversal Design. Part I: Nonlinear Analysis
Modeling Beams with Various Boundary Conditions Using Fully Intrinsic Equations
Rigorous Joining of Advanced Reduced-Dimensional Beam Models to 2-D Finite Element Models
Parametric Study of Joined-Wing Aircraft Geometry
Stability Analysis of Columns with Imperfection
On Static Stability of Damaged Columns
Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft with Fully Intrinsic Equations
Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft
Investigation of the Effect of Damage Shape and Beam Shape Using a Unified Framework
Asymptotic Beam Theory for Planar Deformation of Initially Curved Isotropic Strips
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
AIAA-2004-2025 Effect of Configuration Parameters on the Response and Stability of HAWT's
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