IBRAHIM Mohammed | Department of Aerospace Engineering ,Nagoya University

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概要

• Ibrahim Mohammed K.の詳細を見る
• 同名の論文著者
• Department of Aerospace Engineering ,Nagoya Universityの論文著者

関連著者

• Nakamura Yoshiaki

  Department Of Aeronautical Engineering Nagoya University

• IBRAHIM Mohammed

  Department of Aerospace Engineering ,Nagoya University

• Ibrahim Mohammed

  Department Of Aerospace Engineering Nagoya University

• Nakamura Yoshiaki

  Department Of Aerospace Engineering Nagoya University

• Nakamura Yoshiaki

  Department Of Aerospace Eng. Nagoya University

• IBRAHIM Mohammed

  Department of Aerospace Engineering, Nagoya University

• MORI Koichi

  Department of Aerospace Engineering, Nagoya University

• NAKAMURA Yoshiaki

  Department of Aerospace Engineering, Nagoya University

• NAKAMURA Yoshiaki

  Aerospace Engineering Department, Graduate School of Engineering, Nagoya University

• El-ghandour Mohamed

  Department Of Aerospace Engineering Nagoya University

• Ibrahim Mohammed

  Aerospace Engineering Department Faculty Of Engineering University Of Cairo

• Nakamura Yoshiaki

  Aerospace Engineering Department Graduate School Of Engineering Nagoya University

• Mori Koichi

  Aerospace Engineering Department Graduate School Of Engineering Nagoya University

• EL-GENDI Mahmoud

  Department of Aerospace Engineering, Nagoya University

• Doi Katsunori

  Department Of Aerospace Engineering Nagoya University

• 中村 佳朗

  名古屋大学 工学部

• EL-GHANDOUR Mohamed

  Department of Aerospace Engineering, Nagoya University

• DOI Katsunori

  Department of Aerospace Engineering, Nagoya University

• EL-GHANDOUR Mohamed

  Graduate School of Engineering, Department of Aerospace Engineering, Nagoya University

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著作論文

• Energy Separation in High Subsonic Turbine Cascade
• Novel Flow Control Method for Vortex Shedding of Turbine Blade
• Control of Leakage Flow by Triple Squealer Configuration in Axial Flow Turbine
• Correlation between Linear Stability Theory and Transition of Compressible Jet Shear Layer
• Comparison between Hot and Cold Flow Conditions of Turbine Cascade
• Effects of Tip Cavity Depth, Width, and Location on the Leakage Flow in an Axial Turbine Cascade

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