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Werkstoff
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Parametric Study of Joined-Wing Aircraft Geometry
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
On Static Stability of Damaged Columns
Stability Analysis of Columns with Imperfection
Effect of Engine Placement on Aeroelastic Trim and Stability of Flying Wing Aircraft
Asymptotic Beam Theory for Planar Deformation of Initially Curved Isotropic Strips
Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft with Fully Intrinsic Equations
Investigation of the Effect of Damage Shape and Beam Shape Using a Unified Framework
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-2006-1656 Modeling of Ground Vibration Testing for Highly Flexible Aircraft
AIAA-2004-1837 Structural Optimization of Composite Rotor Blades
AIAA-2004-1650 A Simple Thermopiezoelastic Model for Composite Shells with Accurate Stress Recovery
AIAA-2004-2025 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