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Effects of the novel rib layouts on the tip leakage flow pattern and heat transfer performance of turbine blade

https://doi.org/10.1177/0954410020910883
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Inferred edges come from two machine sources: sweeps of open repository metadata (mostly SSRN and Zenodo), and a bulk OpenAlex citation snapshot. Every row below is labelled with the one it came from. Neither is a complete citation index — absence here is not evidence of absence.

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What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1016/j.applthermaleng.2018.10.093openalex-snapshot
Influences of a multi-cavity tip on the blade tip and the over tip casing aerothermal performance in a high pressure turbine cascade
inferredcites →https://doi.org/10.1016/j.applthermaleng.2019.113976openalex-snapshot
Influence of wear damages on aerodynamic and heat transfer performance in squealer tip gap
inferredcites →https://doi.org/10.1016/j.energy.2017.07.047openalex-snapshot
Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2004.07.029openalex-snapshot
Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2016.07.058openalex-snapshot
Numerical investigations into the effect of squealer–winglet blade tip modifications on aerodynamic and heat transfer performance
inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2019.05.064openalex-snapshot
Effects of the squealer winglet structures on the heat transfer characteristics and aerodynamic performance of turbine blade tip
inferredcites →https://doi.org/10.1115/1.1311285openalex-snapshot
Time-Averaged Heat Flux for a Recessed Tip, Lip, and Platform of a Transonic Turbine Blade
inferredcites →https://doi.org/10.1115/1.1471523openalex-snapshot
Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer
inferredcites →https://doi.org/10.1115/1.1565096openalex-snapshot
Heat Transfer Coefficients and Film-Cooling Effectiveness on a Gas Turbine Blade Tip
inferredcites →https://doi.org/10.1115/1.1643385openalex-snapshot
Effect of Blade Tip Geometry on Tip Flow and Heat Transfer for a Blade in a Low-Speed Cascade
inferredcites →https://doi.org/10.1115/1.2835630openalex-snapshot
Heat Transfer and Effectiveness on Film Cooled Turbine Blade Tip Models
inferredcites →https://doi.org/10.1115/1.4002424openalex-snapshot
Turbine Blade Tip Heat Transfer in Low Speed and High Speed Flows
inferredcites →https://doi.org/10.1115/1.4035175openalex-snapshot
Cooling Injection Effect on a Transonic Squealer Tip—Part I: Experimental Heat Transfer Results and CFD Validation
inferredcites →https://doi.org/10.1115/1.4035200openalex-snapshot
Cooling Injection Effect on a Transonic Squealer Tip—Part II: Analysis of Aerothermal Interaction Physics
inferredcites →https://doi.org/10.1115/1.4036677openalex-snapshot
Effects of Tip Gap Size on the Aerodynamic Performance of a Cavity-Winglet Tip in a Turbine Cascade
inferredcites →https://doi.org/10.1115/1.4037056openalex-snapshot
A Novel Suction-Side Winglet Design Philosophy for High-Pressure Turbine Rotor Tips
inferredcites →https://doi.org/10.1115/90-gt-154openalex-snapshot
Prediction of Tip-Leakage Losses in Axial Turbines
inferredcites →https://doi.org/10.1115/gt2018-75911openalex-snapshot
Heat Transfer Coefficient and Film Cooling Effectiveness on the Partial Cavity Tip of a Gas Turbine Blade
inferredcites →https://doi.org/10.1115/gt2018-75915openalex-snapshot
Numerical Study of Blade Tip Cooling at High Speed With Tip and Pressure-Side Coolant Injections
inferredcites →https://doi.org/10.1115/tbts2013-2072openalex-snapshot
Measurement of Blade Tip Heat Transfer and Leakage Flow in a Turbine Cascade With a Multi-Cavity Squealer Tip
inferredcites →https://doi.org/10.1177/0954410016683735openalex-snapshot
Aerodynamic optimisation of a winglet-cavity tip in a high-pressure axial turbine cascade
inferredcites →https://doi.org/10.1201/b13616openalex-snapshot
Gas Turbine Heat Transfer and Cooling Technology
inferredcites →https://doi.org/10.2514/1.55134openalex-snapshot
Overtip Choking and Its Implications on Turbine Blade-Tip Aerodynamic Performance
inferredcites →https://doi.org/10.2514/1.b35331openalex-snapshot
Aerothermal Performance of Shroudless Turbine Blade Tips with Relative Casing Movement Effects
inferredcites →https://doi.org/10.2514/4.102639openalex-snapshot
Turbine Aerodynamics, Heat Transfer, Materials, and Mechanics
inferredcites →https://doi.org/10.2514/6.2014-2249openalex-snapshot
Numerical study of spallation phenomenon in an arc-jet environment

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

inferred← citeshttps://doi.org/10.2139/ssrn.4135170openalex-extracted
Effect of Multiple Ribs and Tip Injection on the Aerothermal Characteristics of the Squealer Tip in Turbine Stage
inferred← citeshttps://doi.org/10.2139/ssrn.4587567openalex-extracted
inferred← citeshttps://doi.org/10.1007/s11630-022-1683-4openalex-snapshot
Effect of Squealer Tip with Deep Scale Depth on the Aero-thermodynamic Characteristics of Tip Leakage Flow
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2022.119631openalex-snapshot
Effect of multiple cavities and tip injection on the aerothermal characteristics of the squealer tip in turbine stage
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2025.126357openalex-snapshot
Effect of blade rotation on aerothermal characteristics of blade tip with different cavity scales
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2026.131253openalex-snapshot
Film cooling and aerothermal performance of the turbine blade squealer tip with trenched film holes
inferred← citeshttps://doi.org/10.1016/j.ast.2024.109283openalex-snapshot
Numerical investigations on film cooling effectiveness and heat transfer performance of inclined film hole on the turbine blade squealer tip with plasma actuation
inferred← citeshttps://doi.org/10.1016/j.cja.2023.04.015openalex-snapshot
Control of squealer-tip leakage flow with perforated-rib coolant injection in an axial turbine cascade
inferred← citeshttps://doi.org/10.1063/5.0082196openalex-snapshot
Control strategies for tip leakage vortex using inclined squealer rim in axial turbines
inferred← citeshttps://doi.org/10.1080/01457632.2024.2368424openalex-snapshot
Effects of the Slotted-Cavity Tip on the Vortices and Aerothermal Performance in the High-Pressure Turbine
inferred← citeshttps://doi.org/10.1115/1.4054166openalex-snapshot
Effects of Rib Design on the Unsteady Tip Heat Transfer Amplitude for a Turbine Rotor Blade
inferred← citeshttps://doi.org/10.1177/09576509211040328openalex-snapshot
Effect of casing purge flow on heat transfer and cooling performance of blade squealer tip for a gas turbine stage
inferred← citeshttps://doi.org/10.1177/09576509221115906openalex-snapshot
Effects of inclined squealer rims on tip leakage vortex and loss in a transonic axial turbine
inferred← citeshttps://doi.org/10.1177/09576509231167628openalex-snapshot
Modifications of double-rim geometry to improve thermal performance of squealer tip in a turbine stage
inferred← citeshttps://doi.org/10.2478/amns-2025-0652openalex-snapshot
Research on TMD collision damping based on two-way dense ribbed cavity building cover
inferred← citeshttps://doi.org/10.3390/en18225930openalex-snapshot
Advances in the Aerothermal Performance Enhancement of Turbine Blade Tip Configurations
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