IMAIZUMI Takahiro | Department of Aerospace Engineering, Nagoya University
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概要
Department of Aerospace Engineering, Nagoya University | 論文
- Energy Separation in High Subsonic Turbine Cascade
- Novel Flow Control Method for Vortex Shedding of Turbine Blade
- Comparison between Hot and Cold Flow Conditions of Turbine Cascade
- Control of Leakage Flow by Triple Squealer Configuration in Axial Flow Turbine
- Correlation between Linear Stability Theory and Transition of Compressible Jet Shear Layer