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

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

Characterization of Frequency Response of Pressure-Sensitive Paints

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

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.

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

Analysis of Shock-Wave Structures in a Supersonic Biplane by Focusing Schlieren Technique

Development of a Low-Density Wind Tunnel for Simulating Martian Atmospheric Flight

講演・口頭発表等

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
Development of Fast-Response PSP for Surface Pressure Measurement on Airfoils of the Mars Airplane
Fundamental Study of Two-color AA-PSP for Surface Pressure Measurement on Free-flight Projectile
Study on Aerodynamic Characteristics of Airfoils at Supersonic Flight in the Martian Atmospheric Environment
Fundamental Study on the Effects of Shock Wave Interaction on Structures
A Fundamental Study of the Effects of Shock Wave Action on Structures
Basic Research for Quantitative Visualization of Flow Field around Free-Flight Projectiles by Point Diffraction Interferometer
Basic Research of Two-color AA-PSP for the Application to the High-speed Fluid Phenomena
Development of an Automatic Painting System to Support Stable Coating of PSP and TSP on Test Models
衝撃波管による基礎空力試験実施のための感温塗料計測手法の開発
超高速応答型感圧塗料を用いた衝撃波現象の可視化に関する研究
点回折干渉法による衝撃波現象の可視化に関する基礎研究
Basic Research on the Surface Pressure Measurement Method for Hypersonic Projectiles Using Unsteady PSP
Study on Coating Method to Control the Thickness of TSP Layer
Experimental Investigation of Basic Characteristics of CNT Heater for Development of cnt-PSP