Department of Aeronautics and Astronautics, Faculty of Engineering
Department of Aeronautics and Astronautics, Graduate School of Engineering
Department of Aeronautics and Astronautics, School of Engineering
This laboratory aims to develop high-performance CFD technique for all flow mach numbers, i.e. incompressible flow around a wind turbine, transonic flow around an airplane and supersonic/hypersonic flow around a planet-entry vehicle, including the development of modeling complex flow phenomena.
Ground test of Heat Protection System with Arc-heated Wind Tunnel