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

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

Application of digital phase-shift holographic interferometry to weak shock waves propagating at Mach 1.007

Application of laser-induced thermal acoustics in air to measurement of shock-induced temperature changes

Detached shock waves around cylinders flying at mach number ranging from 1 to 2

Visualization and force measurement of high-temperature, supersonic impulse jet impinging on baffle plate

講演・口頭発表等

5cm×5cmデトネーション駆動型爆風シミュレータ測定部での物体に作用する圧力および変形量計測の試み
ロータリーデトネーションの物理メカニズムの解明
背景型シュリーレン法の波面補償に着目した超望遠高精度可視化計測~接地境界層における屈折率構造定数Cn2の計測に向けた検討~
前向き空洞前面での衝撃波振動遷移の数値解析的研究
離脱衝撃波脈動を利用した超音速飛行体の姿勢制御
点回折干渉計によるデトネーション波詳細構造可視化計測
5cm×5cmデトネーション駆動型爆風模擬装置測定部における流れ場の評価
背景型シュリーレン法による高速熱流体現象の3次元温度分布計測
補償光学型BOS法のためのシンチレーション計測による接地境界層の大気じょう乱評価
補償光学型BOS法光学系の試作と空間分解能向上の確認
Al‐CO2デトネーションに向けた粒子拡散の最適化
ディスク型燃焼器を用いた回転デトネーションエンジンに関する研究
5cm×5cmデトネーション駆動型爆風模擬装置測定部における流れ場の可視化
Research on Development of Gas Turbine Engine Using Rotating Detonation Engine
高速度BOS法(Hi‐BOS)による超音速自由飛行体周囲の流れ場可視化
地中式火薬庫模型庫口からの爆風伝播の方位角特性の可視化計測
膨張波管により生成される超高速気流の数値解析
デトネーション駆動型爆風シミュレータ製作に向けた基礎検討
Nonequilibrium Analysis for Utilization of ISAS Expansion tube
Shock Wave Visualization around High‐Speed Projectiles by using Background‐Oriented Schlieren