Numata Daiju

准教授
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

詳細情報

研究キーワード

Flow Visualization

研究分野

Aerospace, marine, and maritime Engineering Aerospace engineering

論文

Effect of Spray Coating Parameters on the Characteristics of Dye-Painted Anodized Aluminum Pressure-Sensitive Paint

DEVELOPMENT OF UNSTEADY PRESSURE-SENSITIVE PAINT FOR LOW REYNOLDS NUMBER WIND TUNNEL TESTS IN LOW-PRESSURE ENVIRONMENTS

Visualization of Pressure and Skin-Friction Fields on Rotating Blade Under Low-Pressure Conditions

Supersonic Ejector-Driving System under Low Pressure: A Performance Evaluation

Correction to: Experimental analysis of transonic buffet on a 3D swept wing using fast-response pressure-sensitive paint (Experiments in Fluids, (2018), 59, 6, (108), 10.1007/s00348-018-2565-5)

Surface flow visualization techniques for analysis on mars-helicopter rotor aerodynamics

Experimental analysis of transonic buffet on a 3D swept wing using fast-response pressure-sensitive paint

Polymer/Ceramic Pressure-Sensitive Paint with Reduced Roughness for Unsteady Measurement in Transonic Flow

Surface pressure measurement on supersonic free-flight projectiles using unsteady PSP techniues

Characterization of Frequency Response of Pressure-Sensitive Paints

Ultrafast-Response Anodized-Aluminum Pressure-Sensitive Paints for Unsteady Flow Measurement

Investigation rear-end of flow structures on a 6:1 prolate spheroid by using the magnetic suspension and balance system

Polymer/ceramic PSP with reduced surface roughness for unsteady pressure measurement in transonic flow

Evaluation of Sprayable Unsteady PSP for Application in a Transonic Wind Tunnel

Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows

Nonlinear Lift on a Triangular Airfoil in Low-Reynolds-Number Compressible Flow

Application of PSP technique to near-field sonic boom measurements in a ballistic range

Unsteady PSP measurement of transonic buffet on a wing

Pressure-sensitive paint technique for surface pressure measurements in a low-density wind tunnel.

Time-resolved PSP imaging of unsteady shock-wave phenomena using a high-speed camera

講演・口頭発表等

Effect of Anodized Aluminum Layer Thickness on the Characteristics of Sulfuric Acid Type Dye-Painted AA-PSP
Fabrication of PC-PSP Using Bathophenanthroline Ruthenium Chloride as the Pressure-Sensitive Dye
Basic Research on Dye-Painted AA-PSP Using Bathophenanthroline Ruthenium Chloride as the Pressure-Sensitive Dye
Fundamental Research on a New AA-PSP for Enhancing the Accuracy of Pressure Field Measurements on the Surface of Supersonic Projectiles
Study on the Basic Characteristics of Supersonic Airfoil for Mars Airplane
Effect of Anodized Aluminum Layer Thickness on the Characteristics of Phosphoric Acid Type Dye-Painted AA-PSP
Effect of Painting Parameters on the Characteristics of Dye-Painted AA-PSP Aimed at Visualizing Unsteady Shock Wave Phenomena
Development of dye-painted AA-PSP for measuring unsteady pressure fields induced by shock waves from hypersonic free-flight projectiles
Research on Ultrafast Response Pressure- Sensitive Paint Suitable for Measuring Unsteady Shock Wave Phenomena in Atmospheric Pressure Environments
Development of Dual-Luminophore Pressure-Sensitive Paint for Application in Wind-Tunnel Testing
Effects of Spray Coating Parameters on the Characteristics of Dye-Painted Anodized Aluminum Pressure-Sensitive Paint
Development of Unsteady Pressure-Sensitive Paint for Measuring Pressure Fields on Wing Surfaces in Low-Pressure Environments
Development of Dye-Painted AA-PSP for Application in High-Speed Unsteady Shock Wave Measurement
Development of Anodized-Aluminum Pressure-Sensitive Paint with Dye Adsorption Performed by an Automatic Painting System
Study on Simultaneous Measurement of Various Fluid Information on Free-Flight Objects
Study on Unsteady Aerodynamic Phenomena around Re-entry Vehicles Using Ballistic Range
Visualization of Sonic Boom Phenomena Using Anodized-Aluminum Pressure Sensitive Paint
Basic Research on the Aerodynamic Characteristics of 3-D Wings in the Martian Atmospheric Environment
Effects of Aerodynamic Devices on Airfoil Flow in the Martian Atmospheric Environment