
Aerodynamics (Applied Aerodynamic and Design Lab.)
- Development of Estimation Program for Aerodynamic Characteristics of Smart UAV
- Database Construction Using Aerodynamic Analysis of Rotor Blade Airfoils
- Aerodynamic Performance Analysis and Shape Optimization of a Rotor Blade with Passive Flow Control Devices
- Aerodynamic Analysis Model for Aircraft External Mounting Device at Subsonic flow
- N-S simulations for finite span flapping wing
- Development of a Three-dimensional High-precision Numerical Analysis Model for Fluid-Structure Interaction in Helicopters
- Development of the Rotor System Load Analysis Program
System and Attitude Control (Flight Dynamics Lab.)
- Airship Design Optimization and Flight Mode Research
- Autonomous Flight UAV System Control Technique Research
- Satellite Communication and Mobile Communication Algorithm
- Real-time Control Technique using Embedded System
- Flight Simulator Design and Development
- Integrated Re-entry Aircraft Control System Development
Structural Design (CAE Lab. for Design and Manufacturing, Aircraft Structural Design Lab.)
- Design and Development of Coaxial-Rotor UAV
- Development in Metal Forming Process using CAE Technology
- Development of composite flexure for helicopter hub
- Tube Hydroforming Technology
- Design and Analysis of Aircraft ideal structure
- Sheet Metal Forming and Manufacturing Technology using Flexible Forming Technology
- Design and Analysis of Rigid -Airship Structure
- Thin Sheet Metal Forming Technology by Multi-Stage Deep Drawing Process
- Micro Forming technology for High Precision Micro part using Thin Sheet Strip
- Design and Development of Prototype for Nano Colloidal Damping System
Propulsion Dynamics (Heat Transfer and Turbomachinery Lab., Aerospace Propulsion and Combustion Lab.)
- Analysis for Flow Characteristic of Turbo Pump and Supersonic Turbine
- Analysis for Combustion Ability of Gas Turbine and Liquid Rocket Engine
- Flow Characteristic Visualization of Turbine Cascade
- Research of Hypersonic Propulsion System
- Flow Analysis for Supersonic Nozzle and Turbine
- Development of Parallel Computing for Large-Scale Numerical Analysis
- 3D Full Engine Simulation
- CFD Analysis for Multi-phases Response Flow
- Development of Aircraft Heat Exchanger
- Turbulence/Combustion Analysis Technique Research for Combustion Instability of Propulsion System
- Laser/Electromagnetism Physics based Space Propulsion System Research