Amanote Research
Register
Sign In
Discover open access scientific publications
Search, annotate, share and cite publications
Publications by Daichi Takahashi
Experimental and Numerical Studies on Leading Edge Film Cooling Performance: Effects of Hole Exit Shape and Freestream Turbulence
Related publications
The Effect of High Freestream Turbulence on Film Cooling Effectiveness
Showerhead Film Cooling Performance of a Turbine Vane at High Freestream Turbulence in a Transonic Cascade
Journal of Turbomachinery
Mechanical Engineering
Effect of Hole Configurations on Film Cooling Performance
Numerical Heat Transfer; Part A: Applications
Numerical Analysis
Condensed Matter Physics
Effects of Free-Stream Turbulence and Surface Roughness on Film Cooling
Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades
Effects of Flow Compressibility and Density Ratio on Film Cooling Performance
Journal of Propulsion and Power
Space
Planetary Science
Fuel Technology
Mechanical Engineering
Aerospace Engineering
Effects of Hub Endwall Geometry and Rotor Leading Edge Shape on Performance of Supersonic Axial Impulse Turbine. Part I
Experimental Studies of Film Cooling in Supersonic Combustors
Numerical and Experimental Investigation of the Methane Film Cooling in Subscale Combustion Chamber
