Synonyme wurden verwendet für:
Werkstoff
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keywords:(Werkstoff)
Aeroelastic Analysis and Optimization of a Rigid/Inflatable Wing
AIAA-2001-1290 Simulation of Transonic Limit Cycle Oscillations Using a CFD Time-Marching Method
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-2004-1938 Nonlinear Aeroelastic Modeling by Block-Oriented Identification
AIAA-2004-1944 Nonlinear Aeroelastic Studies on a Joined-Wing with Wing Buckling Effects
AIAA-2004-2004 Finite Element Load Updating for Plates
AIAA-2006-1640 Time Domain Nonlinear Aeroelastic Analysis for HALE Wings
AIAA-2006-1851 Flight-Loads Effects on Free-Play Induced Limit Cycle Oscillation
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
Behavior of Epoxy Nanocomposites under the Vacuum Ultraviolet Irradiation
Body-Flexure Control with Smart Actuation for Hypervelocity Missiles
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
Continuous Dynamic Simulation for Morphing Wing Aeroelasticity
Control Law Design in a Computational Aeroelasticity Environment