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Werkstoff
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Aeroelastic Analysis and Optimization of a Rigid/Inflatable Wing
AIAA-2001-1295 Near-Exact Analytical Solutions to Linear Time-Variant Systems
AIAA-2001-1611 Effect of Compressive Force on Strut-Braced Wing Response
AIAA-2004-1646 Load Updating for Nonlinear Finite Element Models
AIAA-2004-2004 Finite Element Load Updating for Plates
AIAA-2006-1961 Dynamic Fracture Analysis of Adhesively Bonded Joints Using Explicit Methods
AIAA-2006-2068 Stochastic Eigenvalue Problem with Polynomial Chaos
AIAA-2006-2168 On the Static Analysis of Sandwich Panels with Square Honeycomb Core
AIAA-2006-2173 Degraded Strength Prediction of Micro-Cracked Plain Woven Textile Composites
Algorithm Development for Optimization of Arbitrary Geometry Panels Using Curvilinear Stiffeners
A Modified Dynamic Preisach Model for Hysteresis
A Multidisciplinary Analysis Optimization Environment for Wings Having SpaRibs
A Multi-Fidelity Multi-Strategy and Multi-Disciplinary Design Optimization Environment