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

Application of DP-AA-PSP to Unsteady Shock Wave Phenomena Under Ultra-Short Exposure Conditions

A Study on Enhancing Luminescence Intensity of Dye-Painted Anodized-Aluminum PSP for Application to Unsteady Hypersonic Shock Wave Phenomena

Time-Series Measurement of Unsteady Pressure Fields Induced by Shock Waves Under Atmospheric Pressure Conditions Using Pressure-Sensitive Paint

Development of an Unsteady PSP Applicable to Low Reynolds Number and High Mach Number Flows for the Advancement of Supersonic Mars Aircraft

Improvement of Dye- Painted Anodized-Aluminum Pressure-Sensitive Paint for Shock-Induced Unsteady Flow Measurement

Visualization of Shock Wave Phenomena Induced by Supersonic Projectiles Using Dye-Painted Anodized-Aluminum Pressure-Sensitive Paint

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

講演・口頭発表等

Fundamental Study on Two-Color DP-AA-PSP for Pressure Field Measurements on Supersonic Projectiles
Application of Sulfuric-Acid-Type DP-AA-PSP to Aerodynamic Testing
Effect of Titanium Dioxide Particle Size on the Characteristics of PC-PSP
Fundamental Characterization of Sulfuric-Acid-Type DP-AA-PSP
Aerodynamic Testing of a Mars Aircraft Wing Model using PC-PSP
Characterization of RuDPP-Based PC-PSP for Application to Low Reynolds Number Aerodynamic Testing
Prototype Development of Dye-Painted AA- PSP Using Anodized Coatings on Aluminum Alloy
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