NIIOKA Takashi | Institute of Fluid Science, Tohoku University

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概要

• Niioka Takashiの詳細を見る
• 同名の論文著者
• Institute of Fluid Science, Tohoku Universityの論文著者

関連著者

• NIIOKA Takashi

  Institute of Fluid Science, Tohoku University

• Niioka Takashi

  Institute Of Fluid Science Tohoku University

• Sato Yukinori

  Ishikawajima Jet Service Co. Ltd.

• TOH Hidemi

  Ishikawajima Harima Heavy Industries Co. Ltd.

• WATANABE Takeshi

  Ishikawajima Harima Heavy Industries Co. Ltd.

• JU Yiguang

  Department of Mechanical and Aerospace Engineering, Princeton University

• Ju Yiguang

  Department Of Aeronautics And Space Engineering Tohoku University

• Maruta Kaoru

  Institute Of Fluid Science Tohoku University

• 丸田 薫

  東北大学流体科学研究所

• KOBAYASHI Hideaki

  Institute of Fluid Science, Tohoku University

• 丸田 薫

  東北大流体研

• Minato R

  Muroran Inst. Technol. Muroran Jpn

• Hasegawa Susumu

  Institute Of Fluid Science Tohoku Univ.

• Watanabe Hideto

  Ebara Co. Ltd.

• 丸田 薫

  東北大 流体科研

• TAGASHIRA Takeshi

  Ishikawajima Harima Heavy Industries Co., Ltd.

• Maruta Kaoru

  Department of Science and Technology System, Akita Prefectural Univ.

• Niioka T

  Tohoku Univ. Miyagi Jpn

• MARUTA Kaoru

  Institute of Fluid Science, Tohoku University

• Maruta Kaoru

  Department Of Mechanical Engineering Sophia University

• MINATO Ryojiro

  Subaru Research Center

• GUO Hongsheng

  Institute of Fluid Science, Tohoku University

• Guo Hongsheng

  Department Of Aeronautics And Space Engineering Tohoku University:institute Of Fluid Science Tohoku

• Tagashira Takeshi

  Ishikawajima Harima Heavy Industries Co. Ltd.

• Sato Jun'ichi

  Ishikawajima-harima Heavy Industries Co. Ltd.

• Kobayashi Hideaki

  Institute Of Fluid Science Tohoku University

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著作論文

• Numerical Study of NO_x Emission in High Temperature Air Combustion
• Experimental Study on Spray Characteristics of Prefilming Airblast Atomizer
• Influence of Combustor Inlet Conditions on Combustot Exit Gas Peak Temperature Factor (Experiment by using the Combustor with Pressure Atomizing Fuel Nozzles and the Combustor with Airblast Type Fuel Injectors)
• Study on the Correlation of the Altitude Ignition Parameter and Lightoff Air Fuel Ratio for Jet Engine Combustors
• B104 IGNITION TIMES OF n-DECANE DROPLET ARRAY IN HIGH-TEMPERATURE LOW-SPEED AIRFLOW(Droplet/particle combustion-1)
• Numerical Analysis of Combustion around a Strut in Supersonic Airflow

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