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A Coupled Finite Element Analysis of Independently Modeled Substructures by Penalty Frame Method
Advancements of Synthesis, Manufacture and Analysis of Nanocomposites in Korea
AIAA-2001-1399 General Tensor-Based Naghdi's Shell Element with NURBS Surface Representation
AIAA-2004-2020 Layup Optimization with GA for Tapered Laminates with Internal Plydrops
AIAA-2006-1986 Structural Topology Optimization Using Two-Level Dynamic Condensation Scheme
AIAA-2006-2118 Concurrent Multiscale Analysis Using Higher Order Cauchy-Born Rules
AIAA-2006-2120 Fully Flexible Solid Unit Cell Simulation with Recursive Thermostat Chains
AIAA-2006-2121 System Identification by Subdomain Reduction Method
A Lifting Algorithm for Output-only Continuous Scan Laser Doppler Vibrometry
An Asymptotic Approach for the Analysis of Composite Plates Having Interfacial Imperfections
A Refined Semi-Analytic Sensitivity Based on the Mode Decomposition and Neumann Series Expansion
Atomic Oxygen Sensors Based on Nanograin ZnO Films Prepared by Pulse Laser Deposition
Continuous Dynamic Simulation for Morphing Wing Aeroelasticity
Dynamic Analysis for Delaminated Composites Using DKQ Concept Based on Higher-Order Zig-Zag Theory
Effect of Sc on Microstructures and Corrosion Properties of AZ91
Efficient Higher-Order Shell Theory for Laminated Composites
Exfoliation Corrosion Behavior of 2524 Aluminium Alloy
Global/local Analysis of Laminated Composites with Multiple Delaminations of Various Shapes
High-speed laser cutting of lace [2246-19]
Laser cutting parameters for high-speed cutting of net fabrics [2246-06]
Layup Optimization of Laminated Composite Patches Considering Uncertainty of Material Properties
Mechanical Properties of Composite Laminates Patches with an Aluminum Substrate
Mitigation of GEO Satellite Solar Array Surface Charging: Laboratory Experiment
Multiscale Analysis of Micro/Nano Size Honeycomb Structures
Multiscale Model for Polymer-based Nanocomposites Considering Phase Transition Behavior
Nonlinear Aeroelastic Analysis for A Wrinkling Aeroshell/Ballute System
Nonlinear Aeroelastic Methodology for a Membrane-on-Ballute Model with Hypersonic Bow Shock
Postprocess Method Using a Displacement Field of Higher-Order Laminated Composite Plate Theory