Advancements of Aerospace Computational Structure Technology in Korea
A Gradient Accuracy Study for the Adjoint-Based Navier-Stokes Design Method
A High Pressure Fuel Control and its Injection Characteristics
AIAA-2001-1255 10 Million DOF Finite Element Structural Analysis via Internet Super-Computing
AIAA-2001-1256 Node Activation Technique for Finite Element System
AIAA-2004-1532 Spectral Analysis Method for Linear Dynamic Systems
AIAA-2004-2007 Investigation of Instability in Crash Analysis on Various Computing Environments
AIRCRAFT AUTOPILOT DESIGN USING ASYMMETRIC VARIABLE-SPAN WING MORPHING
Aircraft Flight Envelope Determination Using Upset Detection and Physical Modeling Methods
A Multidisciplinary Possibilistic Approach to Light Aircraft Conceptual Design
A Multifrontal Solver Combined with Mesh Partitioners