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

Time-Resolved Visualization of Projectile-Generated Shock Waves Propagating at Hypersonic Speeds Using DP-AA-PSP

Evaluation of the Luminescence Characteristics of Two-Color DP-AA-PSP for Small Pressure Fluctuation Measurements

Application of Dye-Painted Anodized-Aluminum Pressure-Sensitive Paint to Blast-Wave-Relevant Unsteady Pressure-Field Visualization

Airfoil Characterization in Low Reynolds Number Supersonic Flow for the Development of Supersonic Mars Aircraft

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

講演・口頭発表等

Fundamental Study of the Unsteady Pressure Field on the Ground Surface Generated by Projectile-Induced Shock Waves Using DP-AA-PSP
Measurement of Propagating Shock Waves in Shock Tube Experiments Using DP--AAA--PPSP
Aerodynamic Testing of Free-Flight Models in a Ballistic Range Using 3D-Printed Sabots
Development of a Two-Color DP-AA-PSP for Improved Measurement Accuracy