Yamada Gouji | Department Of Advanced Energy The University Of Tokyo

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概要

• YAMADA Goujiの詳細を見る
• 同名の論文著者
• Department Of Advanced Energy The University Of Tokyoの論文著者

関連著者

• Yamada Gouji

  Department Of Advanced Energy The University Of Tokyo

• Fujita Kazuhisa

  Japan Aerospace Exploration Agency

• TAKAYANAGI Hiroki

  Japan Aerospace Exploration Agency

• Matsuno Takashi

  Department Of Mechanical And Aerospace Engineering Tottori University

• Kawazoe Hiromitsu

  Department Of Mechanical And Aerospace Engineering Tottori University

• Suzuki Toshiyuki

  Aerospace Research And Development Directorate Japan Aerospace Exploration Agency

• Suzuki Toshiyuki

  Japan Aerospace Exploration Agency

• SUZUKI Toshiyuki

  Japan Fine Ceramics Center

• YAMADA Gouji

  The University of Tokyo

• MATSUNO Takashi

  Department of Mechanical and Aerospace Engineering, Tottori University

• SUZUKI Toshiyuki

  Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency

• TAKAYANAGI Hiroki

  Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency

• FUJITA Kazuhisa

  Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency

• Obayashi Shigeru

  Institute Of Engineering Mechanics Tsukuba University

• Takayanagi Hiroki

  Aerospace Research And Development Directorate Japan Aerospace Exploration Agency

• Fujita Kazuhisa

  Aerospace Research And Development Directorate Japan Aerospace Exploration Agency

• AGO Shota

  Department of Mechanical and Aerospace Engineering, Tottori University

• KUBO Yuto

  Department of Mechanical and Aerospace Engineering, Tottori University

• SUEMURA Hiroshi

  Department of Mechanical and Aerospace Engineering, Tottori University

• OTSUTA Singo

  Department of Mechanical and Aerospace Engineering, Tottori University

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著作論文

• Development of Shock Tube for Ground Testing Reentry Aerothermodynamics
• Analysis of Shock Layer Radiation from the Vacuum-Ultraviolet to Near-Infrared Regions
• Shock Layer Radiation Analysis using a Hypervelocity Shock Tube (HVST)
• Numerical Analysis on the Nonequilibrium Phenomena of the Electronic Excitation Process behind Hypersonic Shock Waves
• Temperature Measurements of CO2 and CO2 - N2 Plasma Flows around a Blunt Body in an Arc-Heated Wind Tunnel
• Development of a Sensitivity-Adjustable Three-Component Force Balance and Its Application to Wind Tunnel Testing
• Development of a Shock Tube Facility for Nonequilibrium Radiation Studies in Mars Entry Flight Conditions

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