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Film Cooling Measurements for Cratered Cylindrical Inclined Holes
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inferred← citeshttps://doi.org/10.2139/ssrn.3996078openalex-extracted
Experimental Investigation of Hole-Geometry Effect on Unsteady Film Cooling Effectiveness at Turbine Vane Leading Edge
inferred← citeshttps://doi.org/10.1016/j.ast.2026.113546openalex-snapshot
Coupled effects of film-hole geometry and thermal barrier coating application on overall thermal performance
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2024.107868openalex-snapshot
Effect and optimization of geometric parameters and arrangement on film cooling performance of fan-shaped holes based on generalized regression neural network
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2016.07.001openalex-snapshot
The effects of upstream steps with unevenly spanwise distributed height on rectangular hole film cooling performance
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2019.118652openalex-snapshot
Experimental optimization of a fan-shaped film cooling hole with 30 degrees-injection angle and 6-hole length-to-diameter ratio
inferred← citeshttps://doi.org/10.1051/meca/2011006openalex-snapshot
A comparative study of the film cooling hole configuration effects on the leading edge of asymmetrical turbine blade
inferred← citeshttps://doi.org/10.1115/1.2976784openalex-snapshot
Transient Method for Convective Heat Transfer Measurement With Lateral Conduction—Part I: Application to a Deposit-Roughened Gas Turbine Surface
inferred← citeshttps://doi.org/10.1115/1.4023957openalex-snapshot
Effects of Periodic Unsteady Inflow on Film Cooling and Heat Transfer on Highly Loaded High Pressure Turbine Blades With Flow Separation
inferred← citeshttps://doi.org/10.20998/2078-774x.2015.15.07openalex-snapshot
Advanced Methods of the Film Deposition: Influence of the Acceleration of the Main Flow
inferred← citeshttps://doi.org/10.30684/etj.32.4a.17openalex-snapshot
Effect of Holes Arrangement on Effusion Cooling Performance
inferred← citeshttps://doi.org/10.31390/gradschool_dissertations.344openalex-snapshot
Effect of hole configurations on film cooling from cylindrical inclined holes for the application to gas turbine blades
inferred← citeshttps://doi.org/10.31472/ihe.3.2017.02openalex-snapshot
ПЕРСПЕКТИВНЫЕ СХЕМЫ ПЛЕНОЧНОГО ОХЛАЖДЕНИЯ: ВЛИЯНИЕ ВНЕШНЕЙ ТУРБУЛЕНТНОСТИ
inferred← citeshttps://doi.org/10.5098/hmt.6.8openalex-snapshot
A REVIEW OF HOLE GEOMETRY AND COOLANT DENSITY EFFECT ON FILM COOLING
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