2005-01-1713 The Suspension of the Newly Developed Hyundai Sonata
2006-01-1022 Vehicle Stability through Integrated Active Steering and Differential Braking
2012-3050 Separation Control Characteristics of Synthetic Jets with Circular Exit Array
Abrupt Response Criteria for Directional Control AIAA Paper
Advanced Math-Based Engine Calibration and Control System Design
AIAA-2001-1657 Analysis of Nonlinear Aeroelastic Signals
AIAA-2003-5310 Effect of Wheel Feel System Characteristics on Aircraft Handling Qualities
AIAA-2004-5361 Criterion to Select Roll Control Sensitivity of Transport Aircraft with a Wheel
AIAA-2004-5362 An Approach to Feel System Characteristics Selection
AIAA-2004-6120 A Large S-band Antenna for a Mobile Satellite
AIAA-2006-1869 Over the Failure, MLGSST for T-50 Supersonic Jet Trainer
AIAA-2006-2033 Statistical Analysis Tools for Detection of Non-Linearity in Aeroelastic Phenomena
AIAA-2006-5355 Automated Communication, Ocean, and Meteorological Satellite Operational Orbit System
AIAA-2006-5356 Analysis of Wheel Off-Loading Strategy of COMS
AIAA-2006-5359 The Intelligent VoIP Communication System
AIAA-2006-6497 Analysis of Requirements for Directional Dynamics
Analysis of lens array relay in three-dimensional integral imaging system
A Screening Attenuation Evaluation Method for HEV Power Cable
A Travel Demand Prediction Model with Feedback for Jabodetabek Metropolitan Area, Indonesia
Biomimetic Adaptive Airframe Technology (BAAT) for Rotorcraft Design and Optimization
Biomimetic Adaptive Airframe Technology (BAAT) for Rotorcraft Design and Optimization
Closed-loop Active Flow Control of Stall Separation using Synthetic Jets
Criteria to Estimate the Effect of Static Stability Margin on Aircraft HQ
Criterion to Estimate Optimum Lateral Static Stability Margin AIAA Paper
Design and analysis of gratings and diffractive optical elements for displays
Development and Evaluation of User Interfaces for Situation Observability in Life Support Systems
DEVELOPMENT OF “ARIA”, A COMPACT, ULTRA-QUIET PERSONAL ELECTRIC HELICOPTER
DEVELOPMENT OF ``ARIA'', A COMPACT, ULTRA-QUIET PERSONAL ELECTRIC HELICOPTER
Development of Advanced Light-Duty Powertrain and Hybrid Analysis Tool
Electric Field Measurements in Gases Using Cavity Enhanced Polarimetry
Engine Room Lay-out Study for Fuel Efficiency and Thermal Performance