Aeroelastic Characteristics of High-Aspect-Ratio Wing According to Wing Shape
A Gradient Accuracy Study for the Adjoint-Based Navier-Stokes Design Method
A High Pressure Fuel Control and its Injection Characteristics
A high-resolution multi-spectral imaging system for small satellites
A Hybrid Framework of Worst-Case Execution Time Analysis for Real-Time Embedded System Software
AIAA-2001-1232 Optimal Sensor Placement for Dynamic Testing of Large Structures
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-2001-1299 Effect of a Concentrated Mass on the Spinning Free-Free Beam Subjected to a Thrust
AIAA-2001-1311 Characteristics of Rotating Cantilever Beam with a Crack
AIAA-2001-4977 Development of TT&C System for LEO KOMPSAT
AIAA-2002-5605 A Robust Approach to Pre-concept Design of UCAV Considering Survivability