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A Coupled Finite Element Analysis of Independently Modeled Substructures by Penalty Frame Method
Active Load Control of an Articulated Composite Rotor Blade via Dual Trailing Edge Flaps
Advancements of Synthesis, Manufacture and Analysis of Nanocomposites in Korea
AIAA-2001-1255 10 Million DOF Finite Element Structural Analysis via Internet Super-Computing
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 Mode Selection Criterion Based on Flexibility Approach in Component Mode Synthesis
A Multifrontal Solver Combined with Mesh Partitioners
An Asymptotic Approach for the Analysis of Composite Plates Having Interfacial Imperfections
An Efficient Assumed Strain Triangular Solid Element Tailored for Shell Analysis
A Refined Semi-Analytic Sensitivity Based on the Mode Decomposition and Neumann Series Expansion
Dynamic Analysis for Delaminated Composites Using DKQ Concept Based on Higher-Order Zig-Zag Theory
Effect of Unsteady Blade Motion on the Aerodynamic Performance of Micro-Rotorcraft
Efficient Higher-Order Shell Theory for Laminated Composites
Global/local Analysis of Laminated Composites with Multiple Delaminations of Various Shapes
Improvement of a Rotorcraft Preliminary Design Optimization Framework
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
Optimal Design of A Swashplateless Main Rotor Featuring Active Control of Blade Twist