Film cooling from two rows of holes with opposite orientation angles: injectant behavior and adiabatic film cooling effectiveness
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference14 articles.
1. Measured coolant distributions downstream of single and double rows of film cooling holes;Afejuku;ASME J. Eng. Power,1983
2. Film cooling with injection through holes: adiabatic wall temperature downstream of a circular hole;Goldstein;ASME J. Eng. Power,1968
3. Heat transfer coefficients over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method;Ekkad;ASME J. Turbomach.,1997
4. Film cooling effectiveness over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method;Ekkad;ASME J. Turbomach.,1997
5. Behavior of the laterally injected jet in film cooling: measurements of surface temperature and velocity/temperature field within the jet;Honami;ASME J. Turbomach.,1994
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3. Comparisons of Overall Performance Among Double-Jet Film Cooling Holes, Cylinder Holes, and Fan-Shaped Holes;ASME Journal of Heat and Mass Transfer;2023-10-18
4. Effect of oscillating flow on two rows of cooling holes with various configurations on film cooling performance;Numerical Heat Transfer, Part A: Applications;2023-09-13
5. Large Eddy Simulation of Film Cooling: A Review;Energies;2022-11-24
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