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Effects of Impinging Hole Shapes on Double Swirl Cooling Performance at Gas Turbine Blade Leading Edge

https://doi.org/10.1115/gt2018-75445
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inferred← citeshttps://doi.org/10.2139/ssrn.4584087openalex-extracted
Overall Cooling Effectiveness of Blade Leading Edge with Double Swirl Chamber: Effect of Turbulence Intensity and Wall Thickness
inferred← citeshttps://doi.org/10.2139/ssrn.4591504openalex-extracted
inferred← citeshttps://doi.org/10.1007/s11630-022-1550-8openalex-snapshot
Effects of Variable Jet Nozzle Angles on Cross-Flow Suppression and Heat Transfer Enhancement of Swirl Chamber
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2024.122539openalex-snapshot
Effect of film hole diameter and attack angle on the film cooling performance of leading edge with double swirl chamber under crossflow condition
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2020.104923openalex-snapshot
Numerical investigation on the flow and heat transfer in swirl chambers with distributed multi exit slots and dimple/protrusion structure
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2023.106811openalex-snapshot
Influences of nozzle aspect ratio and inlet Reynolds number on flow and heat transfer characteristics for middle double swirl cooling
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2024.107412openalex-snapshot
Analysis of flow characteristics and heat transfer regulations for gas turbine blade middle double swirl cooling under different nozzle numbers
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2024.107752openalex-snapshot
Large eddy simulation on unsteady flow and heat transfer behaviors of double swirl cooling configuration
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2019.07.055openalex-snapshot
Comparison between impingement/effusion and double swirl/effusion cooling performance under different effusion hole diameters
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2022.107907openalex-snapshot
Numerical investigation on conjugate cooling performance of double swirl cooling at vane leading edge
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2025.110008openalex-snapshot
Overall cooling effectiveness of blade leading edge with double swirl chamber: effect of turbulence intensity and wall thickness
inferred← citeshttps://doi.org/10.1016/j.tsep.2025.104214openalex-snapshot
Flow and conjugated heat transfer characteristics of swirl-rib-film composite cooling in gas turbine leading-edge
inferred← citeshttps://doi.org/10.1115/1.4042311openalex-snapshot
Effects of Target Channel Shapes on Double Swirl Cooling Performance at Gas Turbine Blade Leading Edge
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