Numerical analysis on the film cooling of leading edge with laid back holes to determine the optimal angle for the holes
Author:
Affiliation:
1. School of Mechanical Engineering, College of Engineering, University of Tehran, Tehran, Iran
2. Department of Mechanical Engineering, University of Zanjan, Zanjan, Iran
Publisher
Informa UK Limited
Subject
Mechanical Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/14484846.2018.1543075
Reference36 articles.
1. Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes
2. LES of rotational effects on film cooling effectiveness and heat transfer coefficient in a gas turbine blade with one row of air film injection
3. Investigation of various non-linear eddy viscosity turbulence models for simulating flow and pollutant dispersion on and around a cubical model building
4. Film cooling adiabatic effectiveness measurements of pressure side trailing edge cooling configurations
5. Gas Turbine Film Cooling
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1. Effect and optimization of geometric parameters and arrangement on film cooling performance of fan-shaped holes based on generalized regression neural network;International Communications in Heat and Mass Transfer;2024-11
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3. Experimental investigation of hole-geometry effect on unsteady characteristics of film cooling at turbine vane leading edge;International Journal of Thermal Sciences;2022-09
4. Insights into drilling film cooling holes on ceramic-coated nickel-based superalloys;Archives of Civil and Mechanical Engineering;2022-06-08
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