ICAS2016_0535: GENERAL MESSAGE RACES IN DATA DISTRIBUTION SERVICE PROGRAMS FOR AIRBORNE SOFTWARE
Error Estimation and Grid Adaptation Using Euler Adjoint Method
AIAA 2006-1051 Aerodynamic Optimization of Multi-Element Airfoil
Design of a New On-Board Computer for the New KOMPSAT Bus
AIAA 2006-1397 Flow Fields Analysis around Dimpled Cylinders with Spinning
Controller design for Maglev vehicle system with vehicle-guideway interaction [6794-20]
Analysis on the Long-term Orbital Evolution and Maintenance of KOMPSAT-2
Discrete Adjoint Method for Unstructured Navier-Stokes Solver
Alternative Formulations for Optimization-based-Digital Human Motion Prediction
Aerodynamic Design Optimization of Wing-Body Configurations
F2008-06-059 DEVELOPMENT OF LNT (LEAN NOX TRAP) SYSTEM USING 2ND INJECTOR