MIZUKAKI TOSHIHARU
- 教授
- 学位:博士(工学)
基本情報
所属
- Undergraduate School of Engineering / Department of Aeronautics and Astronautics Aerospace Course
- Graduate School of Science and Technology / Course of Science and Technology
- Graduate School of Engineering / Course of Mechanical Engineering
ジャンル
- Nuclear & Nuclear Power
- Space Development
- Simulation
研究と関連するSDGs
詳細情報
研究キーワード
- Shockwaves
- Fluid Dynamics
- Flow Visualization
- Detonation
- Explosions
- Adaptive Optics
研究分野
- Aerospace, marine, and maritime Engineering Aerospace engineering
- Manufacturing technology (mechanical, electrical/electronic, chemical engineering) Fluid engineering
- Social infrastructure (civil Engineering, architecture, disaster prevention) Disaster prevention engineering Explosion Safety
- Natural sciences Astronomy Adaptive Optics
- Life sciences Biomedical engineering
- Life sciences Biomaterials
論文
Dependence of premixture jet height on detonation wave propagation inside a pressure gain combustion channel
nterferometric visualization of detonation waves inside a pressure gain combustion channel at low-mass flow rates
Numerical analysis of detonation wave propagation in a closed linear combustor with doublet injectors at low plenum pressure
Quantification and visualization of acoustic disturbance inside a supersonic forward-facing cavity: A simplified supersonic-parachute model
Development of a high efficiency system with a rotating detonation engine for a gas turbine engine (RDE-GTE) using pressure gain combustion
Transition behavior of shock waves from oscillation to pulsation around a forward-facing concave with spike
Characteristics of self-sustained-shock pulsation around a forward-facng concave with spike
Shock Wave Oscillation around a Forward-Facing Concave
Numerical investigations on shock oscillations ahead of a hemispherical shell in supersonic flow
Visualization of stagnation point inside the closed wake of a 20%-truncated plug nozzle at starting process
Experimental investigation of unsteady shock oscillation by a forward-facing hemisphere at mach 3
Oscillation characteristics of the shock waves around a supersonic deceleration-device model with aerospike
Quantitative visualization of the development of the blast structure generated by a 0.5 g-PETN pellet using background-oriented schlieren within an explosion chamber
Background-oriented schlieren for large-scale and high-speed aerodynamic phenomena
Development of background-oriented schlieren for NASA langley research center ground test facilities
Background-oriented schlieren with natural background for quantitative visualization of open-air explosions
Visualization of flow separation around an atmospheric entry capsule at low-subsonic mach number using background-oriented schlieren (BOS)
Flow visualization of starting process of a two-dimensional truncated plug nozzle using shock tube
Visualization of compressible vortex rings using the background-oriented schlieren method
講演?口頭発表等
- Numerical and experimental study of actuation characteristics on H2/Air non-premixed rotating detonation engine
- Optical observation on combustion Instability in Rotating Detonation engine
- Flow Viualization Around High-Speed Projectile with Point-Diffraction Interferomety
- Numerical Analysis of Propagation of Detonation Wave Plunging Entry the Fuel Jet Train inside Rotating Detonation Combustor
- Improvement of Spatial Resolution of High-speed-Background Oriented Schlieren through Atmospheric Turbulence
- Mixture Distribution of Solid-Gas-Two-Phase Flow for Gaseous Detonation with Aluminium Particles
- Numerical Analysis of the Influence of Mixing on Detonation Wave Propagation inside a Rotating Detonation Engine by Using Linear Detonation Channel
- Global overpressure measurement for blast loading assessment
所属学会
- JAPAN EXPLOSIVES SOCIETY
- American Institute of Aeronautics and Astronautics
- THE VISUALIZATION SOCIETY OF JAPAN
- THE JAPAN SOCIETY OF FLUID MECHANICS
- THE JAPAN SOCIETY OF MECHANICAL ENGINEERS
- THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
共同研究?競争的資金等の研究課題
Temperature and velocity measurement on unsteady high-Reynolds number flow by using laser-induced thermal acoustics
ResearchMapへ移動します
Contact Us
Inquiries about coverage
Public Affairs Division Public Affairs and Communications Department
Tel. 0463-63-4670(direct dialing)