Research Field
Aerodynamic analysis and design by CFD(Computational Fluid Dynamics) simulation and wind tunnel experiment.
- Advanced Numerical Method
- Aerodynamic Design Optimization
- Experimental/Numerical Active Flow Control
- Integrated Fluid-Structure Simulation of a Liquid Rocket Engine Nozzle Interior
- Experimental/Numerical Biomimetic Aerodynamics
- Flow Physics around a Supersonic Inlet
- Multiphase Flow Simulation
- Hypersonic Flow Simulation
- Machine Learning-Based Numerical Simulation
Research Facilities
Experimental Equipments
- AeroLab company product, 87 series (1961)
- Test section : 1350mm * 950mm
- Maximum speed : 75m/s
- ANOMAX company product (1980)
- Intermittent blowdown type
- Test section : 200mm * 200mm
- Mach number : 2.0, 3.0, 3.8
- Phantom company product, Miro C110
- 1.3 Megapixel, 2/3 inch CMOS sensor
- Supports up to 1,295 fps at 1280x720 resolution
- Supports up to 52,445 fps depending on resolution.
- Universal Laser Systems company product, VLS 6.60
- 60W CO2 laser
- Operating section : 813 x 457 mm
- Used for cutting and marking wood, acrylic, etc.
- Litron Lasers company product, Nano L 200-15 PIV
- Repetition Rate : 0-15 Hz
- Output Energy at 532 nm : 200 mJ
- Beam diameter : 6.5 mm
- Stratasys company product, F170
- FDM system
- Operating section : 254 x 254 x 254 mm
- Avaliable materials : ABS-M30, PLS, ASA, FDA TPU 92A
High-Performance Computing (HPC) Machines
Information of HPC Machines
| Cluster Name | Number of nodes/CPUs Performance | CPU types | Network system |
|---|---|---|---|
| Linux-based Cluster #1 | 103 / 2808 131.8TFlops | Computing node : Intel Xeon E5-2450 V2 (16 Cores) * 8 Intel Xeon E5-2450 V3 (20 Cores) * 8 Intel Xeon E5-2450 V4 (24 Cores) * 60 Intel Xeon Gold 6230 V4 (40 Cores) * 27 | Dual Network (Infiniteband / Gigabit) |
| Linux-based Cluster #2 | 48 / 484 4.8TFlops | Computing node : Intel Xeon E5620 (8 Cores) * 23 Intel Xeon E5649 (12 Cores) * 25 | Gigabit Network |
