山田 剛治

Yamada Gouji

  • 准教授
  • 学位:博士(科学)

基本情報

所属

  • Undergraduate School of Engineering / Department of Mechanical Engineering
  • Graduate School of Science and Technology / Course of Science and Technology
  • Graduate School of Engineering / Course of Mechanical Engineering

詳細情報

研究分野

  • Aerospace, marine, and maritime Engineering Aerospace engineering

受賞

  • Tottori University Scientific Research Award at Tottori Univesity Development of a Shock Tube Facility for Nonequilibrium Radiation Studies in Mars Entry Flight Conditions
  • The Japan Society for Aeronautical and Space Sciences Young Researcher Award Shock Layer Radiation Analysis using a Hypervelocity Shock Tube (HVST), Analysis of Shock Layer Radiation from the Vacuum-Ultraviolet to Near-Infrared Regions

論文

Quasi-0D-Model Mapping of Reflected Shock Tunnel Operating Conditions

Multipoint Spectroscopic Diagnostics of Plasma

Investigation of Aerodynamic Heating under Hypersonic

Mapping of stagnation conditions in reflected shock tunnels

Experimental and numerical study on radiating shock tube flows for spacecraft reentry flights

Shock tube study of nonequilibrium plasma flows in a Mars entry flight condition

Aerodynamic characteristics and flow field of delta wings with the canard

Flow Characterization of CO2-N2-Ar Plasma in a Hollow Electrode Arc Heater

Optical Diagnostics of Shock-induced Argon Plasmas Based on a Simple Collisional-Radiative Model

Aerodynamic Characteristics of a Deployable-Wing Airplane with an Elevon for Mars Exploration

Vectored Jet Control for Trielectrode Plasma Actuator with Serrated Electrode

火星探査に向けた展開翼型惑星探査航空機の高速空力特性

Electron density measurements bedhind a hypersonic shock wave in argon

Spectroscopic Flow Evaluation of Nonequilibrium CO2-Ar Plasma Flow in an Arc-jet Facility

Temperature Evaluation of CO2-N2-Ar Plasma Flows Using the Area Intensity Method

Improvement of a Sensitivity-Adjustable Three-Component Force Balance and Its Application to Supersonic Wind Tunnel Testing

Generation Mechanism of Precursor Electrons ahead of a Hypersonic Shock Wave in Argon

On the mechanism of bluff body flow control by pulsed plasma actuator

Development of a Shock Tube Facility for Nonequilibrium Radiation Studies in Mars Entry Flight Conditions

Temperature Measurements of CO2 and CO2 - N2 Plasma Flows around a Blunt Body in an Arc-Heated Wind Tunnel

講演・口頭発表等

  • Precursor phenomena ahead of a re-entry vehicle into Earth atmosphere
  • Nonequilibrium Radiation of Shock-heated Plasmas with Precursor phenomena
  • Internal energy relaxation processes of nitrogen plasmas at different electronic states in an entry flight condition
  • Spectroscopic Measurement of Plasma Flow with Ablation in an Arc-Heated Wind Tunnel
  • Spectroscopic Evaluation of High Enthalpy Plasma Flows for Heat Shield Material Testing
  • Internal Energy Relaxation Process of Nitrogen Plasma in an Entry Flight
  • Aerodynamic Characteristics and Flow Field of Delta Wings with the Canard
  • Thermochemical Process of Nonequilibrium Plasma Flows In a Mars Entry Flight Condition
  • AMATERAS, The New Type Rail-Gun System
  • Analysis of the thermochemical process in the shock layer generating around space vehicles entering into the Earth atmosphere
  • Spectroscopic Measurements of Plasma Flows with Ablation in an Arc-Heated Wind Tunnel
  • Radiation Characteristics of a Shock induced Argon Plasma with Precursor phenomenon
  • Aerodynamic Characteristics of a Variable-Wing Glider for Planetary Exploration
  • Aerodynamic Characteristics and Flow Field of Delta Wings with the Canard
  • Shock Layer Radiation Analysis for Spacecraft Reentry Flights
  • Spectroscopic Analysis of Shock Layer Flows in a High Enthalpy Arcjet Facility
  • プリカーサ現象を伴う衝撃波アルゴンプラズマの放射特性
  • Flow Characteristics of CO2-N2 Plasma in the Hollow Electrode Arc Heater
  • Analysis of CO2-N2 Plasma Flow in the Discharge Chamber of an Arc Heating Wind Tunnel
  • Extension of the collisional-radiative model to low ionized and low temperature argon plasma for material surface modification

所属学会

  • The American Institute of Aeronautics and Astronautics
  • THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

共同研究・競争的資金等の研究課題

Characterization of the surface interaction between hypersonic plasmas and thermal protection materials around space vehicles

Clarification on nonequilibrium thermochemistry around atmospheric entry vehicles using a ultra-fast imaging absorption spectroscopy

Characteristics of hypersonic nonequilbirium ionization flows around atmospheric entry vehicles

Development of an advanced interferometer measurement method for the characterization of ionization flows

Clarification on the effect of precursor electrons on the thermochemical nonequilibrium process behind shock waves

Improvement of prediction accuracy for thermochemical nonequilibrium process around space vehicles entering into carbon dioxide atmosphere

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