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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
A POD-based Reduced Order Design Scheme for Shape Optimization of Air Vehicles
A Review of Soft Body Impact on Composite Structure
A Ritz Approach for Buckling Prediction of Cracked-Stiffened Structures
A Shear-Flexible Beam Element for Linear Analysis of Unsymmetrically Laminated Beams
Buckling and Crack Propagation of Cracked Box Beams
Buckling and Stress Analysis of Curvilinearly Stiffened Plates Using Meshfree Method
Compression After Impact on Honeycomb Core Sandwich Panels with Thin Facesheets, Part 1: Experiments
Compression After Impact on Honeycomb Core Sandwich Panels with Thin Facesheets, Part 2: Analysis
Computation of Actuation Power Requirements for Smart Wings With Morphing Airfoils
Control Law Design in a Computational Aeroelasticity Environment
Damage Detection in a Prestressed Membrane Using a Wavelet-Based Neuro-Fuzzy System
Design Optimization for Minimum Sound Radiation from Point-Excited Curvilinearly Stiffened Panel
Development of Framework for the Design Optimization of Unitized Structures
Development of Framework for Truss-Braced Wing Conceptual MDO
Durable Joining Technology for Uniformly-Curved Composite Sandwich Structures
Dynamic Stability of Laminated Composite Beams Subject to Subtangential Loads
Effect of Compressive Force on Flutter Speed of a Strut-Braced Wing
Flow Induced Vibrations of Pressure/Temperature Sensors
Flutter Modeling and Suppression for a Strut-Braced Wing
Free Vibration of Thick Generally Laminated Quadrilateral Plates with Point Supports
Generalized Linear Random Vibration Analysis Using Auto-Covariance Orthogonal Decomposition
Grid-Stiffened Panel Optimization Using Curvilinear Stiffeners
Integrated Local Petrov-Galerkin Sinc Method for Structural Mechanics Problems
Karhunen-Loeve Expansion of Non-Gaussian Random Process AIAA Paper 2007-1943 CD-ROM Number 7
Micro-Structural Modeling of 2-D Plain Woven Textile Composites