山田 剛治

山田 剛治

ヤマダ ゴウジ

  • 准教授
  • 学位:博士(科学)

基本情報

所属

  • 工学部 / 機械工学科
  • 総合理工学研究科 / 総合理工学専攻
  • 工学研究科 / 機械工学専攻

詳細情報

研究分野

  • フロンティア(航空・船舶) 航空宇宙工学

受賞

  • 鳥取大学 鳥取大学科学研究業績表彰 Development of a Shock Tube Facility for Nonequilibrium Radiation Studies in Mars Entry Flight Conditions
  • 日本航空宇宙学会 日本航空宇宙学会奨励賞 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

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

担当経験のある科目

  • 機械設計
  • 機械製図
  • 熱力学
  • 流体力学

所属学会

  • アメリカ航空宇宙学会
  • 日本航空宇宙学会

共同研究・競争的資金等の研究課題

プリカーサ現象が大気突入カプセル背面の空力加熱率へ及ぼす影響の解明

大気突入探査機周りの極超音速プラズマ流と熱防御材料の表面相互作用の解明補助事業

極短時間イメージング吸収分光法による大気突入機周り流れの非平衡科学過程の解明

電離流れ場の特性解明のための先進的干渉計測法の開発補助事業

電離流れ場の特性解明のための先進的干渉計測法の開発補助事業

衝撃波前方のプリカーサ電子が衝撃波背後の熱化学的非平衡過程 に及ぼす影響の解明

二酸化炭素大気突入飛翔体まわりで生じる熱化学的非平衡過程の予測精度向上

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