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The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1016/0894-1777(88)90043-xopenalex-snapshot
Describing the uncertainties in experimental results
inferredcites →https://doi.org/10.1016/b978-0-12-381383-1.00002-3openalex-snapshot
Fundamentals of Fluid Mechanics
inferredcites →https://doi.org/10.1016/s0376-0421(02)00031-3openalex-snapshot
Modern developments in shear-stress measurement
inferredcites →https://doi.org/10.1115/1.1397308openalex-snapshot
Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II—Heat Transfer and Film-Cooling Effectiveness
inferredcites →https://doi.org/10.1115/1.1400112openalex-snapshot
Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I—Aerodynamic Measurements
inferredcites →https://doi.org/10.1115/1.1559897openalex-snapshot
Effects of Aeroderivative Combustor Turbulence on Endwall Heat Transfer Distributions Acquired in a Linear Vane Cascade
inferredcites →https://doi.org/10.1115/1.1811099openalex-snapshot
Adiabatic Effectiveness Measurements of Endwall Film-Cooling for a First-Stage Vane
inferredcites →https://doi.org/10.1115/1.2720497openalex-snapshot
The Effects of Varying the Combustor-Turbine Gap
inferredcites →https://doi.org/10.1115/1.2840937openalex-snapshot
Film Cooling With Compound Angle Holes: Heat Transfer
inferredcites →https://doi.org/10.1115/1.2841351openalex-snapshot
Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall
inferredcites →https://doi.org/10.1115/1.2927702openalex-snapshot
Secondary Loss Generation in a Linear Cascade of High-Turning Turbine Blades
inferredcites →https://doi.org/10.1115/1.3230246openalex-snapshot
An Experimental Study of Endwall and Airfoil Surface Heat Transfer in a Large Scale Turbine Blade Cascade
inferredcites →https://doi.org/10.1115/1.3230352openalex-snapshot
Crossflows in a Turbine Cascade Passage
inferredcites →https://doi.org/10.1115/1.3250586openalex-snapshot
Turbulent Transport on the Endwall in the Region Between Adjacent Turbine Blades
inferredcites →https://doi.org/10.1115/1.3262089openalex-snapshot
Predictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades
inferredcites →https://doi.org/10.1115/1.3450239openalex-snapshot
An Experimental Study of Heat Transfer and Film Cooling on Large-Scale Turbine Endwalls
inferredcites →https://doi.org/10.1115/2000-gt-0199openalex-snapshot
Effects of Slot Bleed Injection Over a Contoured Endwall on Nozzle Guide Vane Cooling Performance: Part I — Flow Field Measurements
inferredcites →https://doi.org/10.1115/90-gt-095openalex-snapshot
Prediction and Measurement of Film Cooling Effectiveness for a First-Stage Turbine Vane Shroud
inferredcites →https://doi.org/10.1115/gt2004-53326openalex-snapshot
Adiabatic Effectiveness Measurements of Endwall Film-Cooling for a First Stage Vane
inferredcites →https://doi.org/10.1115/gt2006-90355openalex-snapshot
Migration of Film-Coolant From Slot and Hole Ejection at a Turbine Vane Endwall
inferredcites →https://doi.org/10.1115/gt2006-90580openalex-snapshot
Surface Shear Stress and Pressure Measurements in a Turbine Cascade
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.4641840openalex-extracted
Numerical Study on the Effect of Rim Seal Slot Filleting on Turbine Endwall Cooling Performance
inferred← citeshttps://doi.org/10.1007/s11630-021-1468-6openalex-snapshot
Numerical Investigations of Film Cooling Characteristics of Interrupted Slot and Trench Holes on a Vane Endwall
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2016.08.172openalex-snapshot
Effect of purge flow on endwall flow and heat transfer characteristics of a gas turbine blade
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2018.05.088openalex-snapshot
Effects of location and profile of upstream slot on the endwall aerothermal performance of a gas turbine blade
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2019.114844openalex-snapshot
Study of effects of axisymmetric endwall contouring on film cooling/heat transfer and secondary losses in a cascade of first stage nozzle guide vane
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2023.120435openalex-snapshot
Experimental decoupled-analysis of overall cooling effectiveness for a turbine endwall with internal and external cooling configurations
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2024.122693openalex-snapshot
Numerical investigation on the effect of sealing clearance on endwall film cooling effectiveness under rotating condition
inferred← citeshttps://doi.org/10.1016/j.csite.2024.105211openalex-snapshot
Effect of profiled endwall on nozzle guide vane with coolant purge flow
inferred← citeshttps://doi.org/10.1016/j.energy.2025.139448openalex-snapshot
Optimization of film cooling hole using Genetic algorithm for enhanced turbine endwall cooling performance
inferred← citeshttps://doi.org/10.1016/j.energy.2025.139512openalex-snapshot
Thermal performance degradation induced by transition piece wall thickening in gas turbine
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2021.105585openalex-snapshot
Research on the effect of the swirling coolant within endwall passage on film cooling/heat transfer and aerodynamic losses
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2025.109125openalex-snapshot
Effects of transition piece wall and misalignment on endwall cooling performance in gas turbines
inferred← citeshttps://doi.org/10.1016/j.ijheatfluidflow.2024.109671openalex-snapshot
Experimental and numerical investigation into the effects of spline mid-passage gap on endwall film cooling performance and aerodynamic characteristics
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2012.04.024openalex-snapshot
Influence of flow injection angle on a leading-edge horseshoe vortex
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2016.02.014openalex-snapshot
Numerical study on the effects of slot injection configuration and endwall alignment mode on the film cooling performance of vane endwall
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2017.08.072openalex-snapshot
Effects of upstream slot geometry on the endwall aerothermal performance of a gas turbine blade under different ejection angle conditions
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2017.11.150openalex-snapshot
Experimental and numerical investigations of shaped hole film cooling with the influence of endwall cross flow
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2018.03.038openalex-snapshot
Effects of the cooling configurations layout near the first-stage vane leading edge on the endwall cooling and phantom cooling of the vane suction side surface
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2021.121034openalex-snapshot
Effect of misalignment at 2nd vane endwall on heat transfer with purge flow
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2023.124899openalex-snapshot
Film cooling effectiveness from upstream purge slots of a turbine vane endwall: Experiment, modeling, and correlation
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2020.106805openalex-snapshot
Effects of the positive pre-swirl purge flow on endwall aero-thermal performance of a gas turbine blade
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2021.107140openalex-snapshot
Effect of leakage flow on the endwall cooling performance in high subsonic turbine cascade
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2023.108762openalex-snapshot
A comparative study of purge slot exit shape on the film cooling effectiveness of a gas turbine shroud
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2023.108768openalex-snapshot
Effect of upstream slot leakage on turbine endwall film cooling characteristics
inferred← citeshttps://doi.org/10.1016/j.tsep.2024.102797openalex-snapshot
Effects of rim seal exit geometry on the cooling characteristics of turbine endwall and blade suction side
inferred← citeshttps://doi.org/10.1016/j.tsep.2025.103333openalex-snapshot
Experimental and computational investigation of the regional endwall cooling performance considering influences of film holes layouts and purge slot shape
inferred← citeshttps://doi.org/10.1016/j.tsep.2025.103522openalex-snapshot
Investigation on the cooling characteristic of turbine endwall with mid-passage gap misalignment
inferred← citeshttps://doi.org/10.1063/1.5144418openalex-snapshot
Numerical aero-thermal study of high-pressure turbine nozzle guide vane: Effects of inflow conditions
inferred← citeshttps://doi.org/10.1063/5.0248773openalex-snapshot
Numerical study on the effect of rim seal slot filleting on turbine endwall cooling
inferred← citeshttps://doi.org/10.1080/01457632.2024.2437894openalex-snapshot
Effects of Spline Mid-Passage Gap on Turbine Endwall Film Cooling Characteristics
inferred← citeshttps://doi.org/10.1080/10407782.2020.1835110openalex-snapshot
Endwall film cooling holes design upstream of the leading edge of a turbine vane
inferred← citeshttps://doi.org/10.1115/1.3068316openalex-snapshot
Film-Cooling Flowfields With Trenched Holes on an Endwall
inferred← citeshttps://doi.org/10.1115/1.4002950openalex-snapshot
The Effect of the Combustor-Turbine Slot and Midpassage Gap on Vane Endwall Heat Transfer
inferred← citeshttps://doi.org/10.1115/1.4003725openalex-snapshot
Film Cooling Effect of Rotor-Stator Purge Flow on Endwall Heat/Mass Transfer
inferred← citeshttps://doi.org/10.1115/1.4004817openalex-snapshot
Effects of Orientation and Position of the Combustor-Turbine Interface on the Cooling of a Vane Endwall
inferred← citeshttps://doi.org/10.1115/1.4007602openalex-snapshot
Impact of the Combustor-Turbine Interface Slot Orientation on the Durability of a Nozzle Guide Vane Endwall
inferred← citeshttps://doi.org/10.1115/1.4032165openalex-snapshot
Comparison of the Three-Dimensional Boundary Layer on Flat Versus Contoured Turbine Endwalls
inferred← citeshttps://doi.org/10.1115/1.4032364openalex-snapshot
A New Test Facility to Investigate Film Cooling on a Nonaxisymmetric Contoured Turbine Endwall—Part II: Heat Transfer and Film Cooling Measurements
inferred← citeshttps://doi.org/10.1115/1.4035162openalex-snapshot
Turbine Vane Endwall Film Cooling With Slashface Leakage and Discrete Hole Configuration
inferred← citeshttps://doi.org/10.1115/1.4041342openalex-snapshot
Endwall Film Cooling Performance for a First-Stage Guide Vane With Upstream Combustor Walls and Inlet Injection
inferred← citeshttps://doi.org/10.1115/1.4051416openalex-snapshot
Uncertainty Quantification of Aero-Thermal Performance of a Blade Endwall Considering Slot Geometry Deviation and Mainstream Fluctuation
inferred← citeshttps://doi.org/10.1115/1.4052457openalex-snapshot
Endwall Heat Transfer and Cooling Performance of a Transonic Turbine Vane With Upstream Injection Flow
inferred← citeshttps://doi.org/10.1115/1.4052737openalex-snapshot
Aerodynamics and Heat Transfer Inside a Gas Turbine Mid-Passage Gap
inferred← citeshttps://doi.org/10.1115/1.4063050openalex-snapshot
Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results
inferred← citeshttps://doi.org/10.1615/ihtc17.180-20openalex-snapshot
Effect of upstream misalignment on film cooling effectiveness with purge flow of the nozzle endwall
inferred← citeshttps://doi.org/10.29008/etc2021-484openalex-snapshot
Experimental investigation of the influence of density ratio and vane exit mach number on platform cooling
inferred← citeshttps://doi.org/10.3390/app132312594openalex-snapshot
Numerical Study of Endwall Modification with Micro-Scale Ribs in a Turbine Cascade
inferred← citeshttps://doi.org/10.3390/en16247976openalex-snapshot
Experimental and Numerical Investigations into the Effects of Rim Seal Structure on Endwall Film Cooling and Flow Field Characteristics
inferred← citeshttps://doi.org/10.4028/www.scientific.net/amm.629.119openalex-snapshot
Aerodynamics Performance of Endwall Film Cooling under the Influence of Purge Flow in High Pressure Turbine Cascade
inferred← citeshttps://doi.org/10.5293/kfma.2015.18.6.037openalex-snapshot
Conjugate Heat Transfer Analysis of High Pressure Turbine with Secondary Flow Path and Thermal Barrier Coating
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