Tokyo University of Science
Department of Mechanical and Aerospace Engineering
Faculty of Science and Technology


 


     
Tokyo University of Science
Department of Mechanical Engineering
Faculty of Science and Technology

Ogasawara laboratory



Snapshots of research work and laboratory
Seminar Local Complex Flow
Computational Fluid Dynamics Wind Tunnel Test

Area of expertise
High Speed Aerodynamics
Aerospace Vehicle Flight Mechanics
Space Transportation System

Research theme
Hypersonic Aerothermodynamics
Interaction between Flight Mechanics and High Speed Aerodynamics

Laboratory profile
Realization of fully reusable space launch system is of our interest. The laboratory aims to generate practical technologies by using interaction between flight dynamics and high speed aerodynamics.

Staff
Instractor: Ko OGASAWARA