Amanote Research
Register
Sign In
Discover open access scientific publications
Search, annotate, share and cite publications
Publications by E. R. G. Eckert
Film Cooling of the Gas Turbine Endwall by Discrete-Hole Injection
Related publications
Performance of Gas Turbine Film Cooling With Backward Injection
Energy and Power Engineering
Effects of Surface Deposition, Hole Blockage, and Thermal Barrier Coating Spallation on Vane Endwall Film Cooling
Journal of Turbomachinery
Mechanical Engineering
Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades
The Influences of Off-Design Incidence Angle and Discrete Hole Shapes on Film Cooling Effectiveness
Effect of Film-Cooling Hole Location on Turbulator Heat Transfer Enhancement in Turbine Blade Internal Air-Cooling Circuits
Influence of the Pressure Side Injection Slot on the Cooling Performance of Endwall Surface
Numerical Heat Transfer; Part A: Applications
Numerical Analysis
Condensed Matter Physics
Effect of Hole Configurations on Film Cooling Performance
Numerical Heat Transfer; Part A: Applications
Numerical Analysis
Condensed Matter Physics
Bump and Trench Modifications to Film-Cooling Holes at the Vane-Endwall Junction
Journal of Turbomachinery
Mechanical Engineering
Thermionic Method of Cooling Turbine Blades of Spacecraft Gas Turbine Converters
Engineering Journal: Science and Innovation
