Faculty & staff
Akira OyamaProfessor
Professor, Department of Space Flight Systems, ISAS / JAXA
Aerospace Engineering, Fluid Dynamics, Design Engineering
Students
澤田健D3
Fluid–Structure Interaction Analysis of a Deployable Flexible Aeroshell
渡辺綾乃D3
Feedback Flow Control Using Plasma Actuators
大西龍汰郎D2
Study of Plume–Surface Interaction (PSI) during Soft Landings on Mars
飯田怜央D2
Research on Deployable Flexible Aeroshells
篠塚温志D1
To Be Determined
ペドロ Pedro Domingos VALED1
To Be Determined
飯田悠生M2
Airfoil Optimization for a Micro Mars Airplane
黒田悠哉M2
Research on Mars Helicopters
倉田昇祈M2
Research on CubeSat-Class Spacecraft for Mars Atmospheric Entry
竹内玲温M2
Multiobjective Design Optimization of a Mars Sample Return Rocket Using Hybrid Rocket Engines
中川貴淑M2
Study of Plume–Surface Interaction (PSI) during Soft Landings on Mars
武川光李M1
Numerical Study of Tandem Wings for a Micro Mars Airplane
柳井拓海M1
Study of Autorotation in Mars Multicopters
中森悠太M1
Analysis of Attitude Stability along the Descent Trajectory of a Flexible Aeroshell for Mars Landing Missions
奥友雄梧M1
Conceptual Design of a Tailsitter Mars Airplane
上原里記B4
Multiobjective Design Optimization of a Mars Sample Return Rocket Using Solid Rocket Motors
Collaborators
青山剛史
Computational Fluid Dynamics, Aerodynamics, Aeroacoustics, Hypersonic Vehicles, Capsule Dynamic Stability, Rotorcraft, Model-Based Development
高木亮治
Aerodynamics, Information Technology, Computational Science, Computational Fluid Dynamics
佐藤允
Next-Generation Aircraft, Novel Convertible eVTOL Aircraft, Mars Aircraft, DBD Plasma Actuators, Flow Control
西田浩之
Aerospace Engineering, Plasma Engineering, Compressible Fluid Dynamics
関本諭志
Development of a Nonlinear Flight Simulator for Flight Control Using DBD Plasma Actuators, and Experimental Studies on Separated Flow Control at Low Reynolds Numbers