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Aerodynamic Aspects of Endwall Film-Cooling

https://doi.org/10.1115/96-gt-208
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What this work says

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

inferredcites →https://doi.org/10.1115/1.2836692openalex-snapshot
The Aerodynamic Mixing Effect of Discrete Cooling Jets With Mainstream Flow on a Highly Loaded Turbine Blade
inferredcites →https://doi.org/10.1115/1.2840916openalex-snapshot
Heat Transfer Committee Best Paper of 1995 Award: Distribution of Film-Cooling Effectiveness on a Turbine Endwall Measured Using the Ammonia and Diazo Technique
inferredcites →https://doi.org/10.1115/1.2927692openalex-snapshot
Aerodynamics of Cooling Jets Introduced in the Secondary Flow of a Low-Speed Turbine Cascade
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/10.1115/1.2927981openalex-snapshot
Secondary Flow Measurements in a Turbine Cascade With High Inlet Turbulence
inferredcites →https://doi.org/10.1115/1.2929422openalex-snapshot
Discrete-Jet Film Cooling: A Comparison of Computational Results With Experiments
inferredcites →https://doi.org/10.1115/1.3230713openalex-snapshot
Influence of Mach Number and End Wall Cooling on Secondary Flows in a Straight Nozzle Cascade
inferredcites →https://doi.org/10.1115/1.3239704openalex-snapshot
Recent Progress in the Understanding of Basic Aspects of Secondary Flows in Turbine Blade Passages
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/10.1115/89-gt-187openalex-snapshot
An Experimental Study of Heat Transfer and Film Cooling on Low Aspect Ratio Turbine Nozzles
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/10.1115/91-gt-252openalex-snapshot
Film Cooling Research on the Endwall of a Turbine Nozzle Guide Vane in a Short Duration Annular Cascade: Part 1 — Experimental Technique and Results
inferredcites →https://doi.org/10.1115/93-gt-114openalex-snapshot
Reduction in Secondary Flows and Losses in a Turbine Cascade by Upstream Boundary Layer Blowing
inferredcites →https://doi.org/10.1115/94-gt-067openalex-snapshot
Film Cooling of the Gas Turbine Endwall by Discrete-Hole Injection
inferredcites →https://doi.org/10.1115/95-gt-001openalex-snapshot
Distribution of Film-Cooling Effectiveness on a Turbine Endwall Measured Using the Ammonia and Diazo Technique
inferredcites →https://doi.org/10.2514/6.1972-11openalex-snapshot
Prediction of effects of mass-transfer cooling on the blade-row efficiency of turbine airfoils

What points at this work

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

inferred← citeshttps://doi.org/10.5281/zenodo.1072863openalex-extracted
Hole Configuration Effect On Turbine Blade Cooling
inferred← citeshttps://doi.org/10.1007/s10749-011-0209-5openalex-snapshot
Analysis of physical processes and operating behavior of gas turbine units with high loading of the gas turbine stage
inferred← citeshttps://doi.org/10.1007/s11630-016-0833-3openalex-snapshot
Investigation on cooling effectiveness and aerodynamic loss of a turbine cascade with film cooling
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.2006.10.006openalex-snapshot
Measurements of net change in heat flux as a result of leakage and steps on the contoured endwall of a gas turbine first stage nozzle
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2015.07.082openalex-snapshot
Effect of discrete-hole arrangement on film-cooling effectiveness for the endwall of a turbine blade cascade
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2017.04.143openalex-snapshot
Influence of the upstream slot geometry on the endwall cooling and phantom cooling of vane suction side surface
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2017.10.109openalex-snapshot
Numerical investigations into heat transfer and film cooling effect on a transonic blade endwall
inferred← citeshttps://doi.org/10.1016/j.ast.2019.105654openalex-snapshot
Transient analysis of upstream wake inside turbine blade passage with purge flow
inferred← citeshttps://doi.org/10.1016/j.ast.2020.105923openalex-snapshot
Effects of compound angle on film cooling effectiveness considering endwall lateral pressure gradient
inferred← citeshttps://doi.org/10.1016/j.csite.2018.01.001openalex-snapshot
Film cooling modeling of a turbine vane with multiple configurations of holes
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2014.07.014openalex-snapshot
An experimental investigation of secondary flow characteristics in a linear turbine cascade with upstream converging slot-holes using TR-PIV
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2018.02.031openalex-snapshot
An experimental investigation of cooling characteristics at a vane end-wall with a locally enhanced hole-layout
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2018.03.011openalex-snapshot
Effect of the wake on the heat transfer of a turbine blade endwall according to relative position of the cylindrical rod
inferred← citeshttps://doi.org/10.1016/j.ijheatfluidflow.2006.05.002openalex-snapshot
Influence of hole shape on the performance of a turbine vane endwall film-cooling scheme
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2005.07.036openalex-snapshot
Heat transfer and film-cooling for the endwall of a first stage turbine vane
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2015.06.026openalex-snapshot
Film cooling effectiveness distribution of cylindrical hole injections at different locations on a vane endwall
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.2016.06.047openalex-snapshot
Influence of different film cooling arrangements on endwall cooling
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2016.07.033openalex-snapshot
Effects of the leading edge injection slot on the film cooling and heat transfer performance of the vane endwall
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2018.01.117openalex-snapshot
Computational investigation of film cooling and secondary flow on turbine endwall with coolant injection from upstream interrupted slot
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2018.12.079openalex-snapshot
Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2019.01.093openalex-snapshot
Computational study of film cooling and flowfields on a stepped vane endwall with a row of cylindrical hole and interrupted slot injections
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2018.03.020openalex-snapshot
Influence of coolant mass flow rate on the endwall conjugate heat transfer
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2018.10.019openalex-snapshot
Suppression of endwall heat transfer in the junction region with a symmetric airfoil by a vortex generator pair
inferred← citeshttps://doi.org/10.1029/2000gl011447openalex-snapshot
Heterogeneous reactions in aircraft gas turbine engines
inferred← citeshttps://doi.org/10.1080/10407782.2017.1326788openalex-snapshot
Effects of the layout of film holes near the vane leading edge on the endwall cooling and phantom cooling of the vane suction side surface
inferred← citeshttps://doi.org/10.1080/10407782.2018.1459140openalex-snapshot
Influence of the pressure side injection slot on the cooling performance of endwall surface
inferred← citeshttps://doi.org/10.1080/17686733.2015.1066135openalex-snapshot
Infrared thermography to study endwall cooling and heat transfer in turbine stator vane passages using the auxiliary wall method and comparison to numerical simulations
inferred← citeshttps://doi.org/10.1115/1.1397776openalex-snapshot
Convective Heat Transfer and Aerodynamics in Axial Flow Turbines
inferred← citeshttps://doi.org/10.1115/1.1400113openalex-snapshot
Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint
inferred← citeshttps://doi.org/10.1115/1.1401026openalex-snapshot
Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame
inferred← citeshttps://doi.org/10.1115/1.1811099openalex-snapshot
Adiabatic Effectiveness Measurements of Endwall Film-Cooling for a First-Stage Vane
inferred← citeshttps://doi.org/10.1115/1.2098788openalex-snapshot
Fan-Shaped Hole Effects on the Aero-Thermal Performance of a Film-Cooled Endwall
inferred← citeshttps://doi.org/10.1115/1.2098791openalex-snapshot
Effect of Midpassage Gap, Endwall Misalignment, and Roughness on Endwall Film-Cooling
inferred← citeshttps://doi.org/10.1115/1.2752184openalex-snapshot
Film-Cooling Effectiveness on a Rotating Blade Platform
inferred← citeshttps://doi.org/10.1115/1.2777186openalex-snapshot
Film Cooling Effectiveness Distributions on a Turbine Blade Cascade Platform With Stator-Rotor Purge and Discrete Film Hole Flows
inferred← citeshttps://doi.org/10.1115/1.2812933openalex-snapshot
Bump and Trench Modifications to Film-Cooling Holes at the Vane-Endwall Junction
inferred← citeshttps://doi.org/10.1115/1.2907440openalex-snapshot
Film Cooling Effectiveness Distribution on a Gas Turbine Blade Platform With Inclined Slot Leakage and Discrete Film Hole Flows
inferred← citeshttps://doi.org/10.1115/1.2952365openalex-snapshot
Effect of Upstream Wake With Vortex on Turbine Blade Platform Film Cooling With Simulated Stator-Rotor Purge Flow
inferred← citeshttps://doi.org/10.1115/1.3068316openalex-snapshot
Film-Cooling Flowfields With Trenched Holes on an Endwall
inferred← citeshttps://doi.org/10.1115/1.3072489openalex-snapshot
Aerothermal Performance of Streamwise and Compound Angled Pulsating Film Cooling Jets
inferred← citeshttps://doi.org/10.1115/1.3142860openalex-snapshot
Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique
inferred← citeshttps://doi.org/10.1115/1.3192147openalex-snapshot
Endwall Film Cooling Effects on Secondary Flows in a Contoured Endwall Nozzle Vane
inferred← citeshttps://doi.org/10.1115/1.4003174openalex-snapshot
Heat Transfer for the Blade of a Cooled Stage and One-Half High-Pressure Turbine—Part II: Independent Influences of Vane Trailing Edge and Purge Cooling
inferred← citeshttps://doi.org/10.1115/1.4003426openalex-snapshot
Aerodynamic and Endwall Film-Cooling Investigations of a Gas Turbine Nozzle Guide Vane Applying Temperature-Sensitive Paint
inferred← citeshttps://doi.org/10.1115/1.4004858openalex-snapshot
Influence of Coolant Flow Rate on Aero-Thermal Performance of a Rotor Blade Cascade With Endwall Film Cooling
inferred← citeshttps://doi.org/10.1115/1.4005732openalex-snapshot
Influence of Coolant Density on Turbine Blade Platform Film-Cooling
inferred← citeshttps://doi.org/10.1115/1.4006419openalex-snapshot
Flow Measurements in a First Stage Nozzle Cascade Having Endwall Contouring, Leakage, and Assembly Features
inferred← citeshttps://doi.org/10.1115/1.4006776openalex-snapshot
Heat Transfer for the Film-Cooled Vane of a 1-1/2 Stage High-Pressure Transonic Turbine—Part II: Effect of Cooling Variation on the Vane Airfoil and Inner End Wall
inferred← citeshttps://doi.org/10.1115/1.4025688openalex-snapshot
Single and Multiple Row Endwall Film-Cooling of a Highly Loaded First Turbine Vane With Variation of Loading
inferred← citeshttps://doi.org/10.1115/1.4028024openalex-snapshot
Shower Head and Trailing Edge Cooling Influence on Transonic Vane Aero Performance
inferred← citeshttps://doi.org/10.1115/1.4033292openalex-snapshot
The Combined Effects of an Upstream Ramp and Swirling Coolant Flow on Film Cooling Characteristics
inferred← citeshttps://doi.org/10.1115/1.4035832openalex-snapshot
Influence of Combustor Swirl on Endwall Heat Transfer and Film Cooling Effectiveness at the Large Scale Turbine Rig
inferred← citeshttps://doi.org/10.1115/1.4036361openalex-snapshot
Experimental Investigation of Endwall Heat Transfer With Film and Impingement Cooling
inferred← citeshttps://doi.org/10.1115/1.4038278openalex-snapshot
Film Cooling Effectiveness Comparison on Full-Scale Turbine Vane Endwalls Using Pressure-Sensitive Paint Technique
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/10.1115/1.4045069openalex-snapshot
Design of Full-Scale Endwall Film Cooling of a Turbine Vane
inferred← citeshttps://doi.org/10.1115/1.4045990openalex-snapshot
Transonic Turbine Vane Endwall Film Cooling Using the Pressure-Sensitive Paint Measurement Technique
inferred← citeshttps://doi.org/10.1115/1.4050070openalex-snapshot
Nozzle Passage Endwall Effectiveness Values With Various Combustor Coolant Flowrates—Part 1: Flowfield Velocity and Coolant Concentration Measurements
inferred← citeshttps://doi.org/10.1115/1.4050120openalex-snapshot
Experimental Investigation of Film Cooling Performance on Blade Endwall With Diffusion Slot Holes and Stator–Rotor Purge Flow
inferred← citeshttps://doi.org/10.1115/1.4050917openalex-snapshot
Implementation of Rectangular Vortex Generator Pairs to Improve Film Cooling Effectiveness on Transonic Rotor Blade Endwall
inferred← citeshttps://doi.org/10.1115/2001-gt-0145openalex-snapshot
Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I — Aerodynamic Measurements
inferred← citeshttps://doi.org/10.1115/98-gt-483openalex-snapshot
The Design of an Improved Endwall Film-Cooling Configuration
inferred← citeshttps://doi.org/10.1115/gt2002-30189openalex-snapshot
Prediction and Measurement of the Flow and Heat Transfer Along the Endwall and Within an Inlet Vane Passage
inferred← citeshttps://doi.org/10.1115/gt2003-38252openalex-snapshot
Computational Predictions of Endwall Film-Cooling for a First Stage Vane
inferred← citeshttps://doi.org/10.1115/gt2006-90684openalex-snapshot
Endwall Film Cooling Through Fan-Shaped Holes With Different Area Ratios
inferred← citeshttps://doi.org/10.1115/gt2008-50286openalex-snapshot
Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling
inferred← citeshttps://doi.org/10.1115/gt2013-94943openalex-snapshot
Aerodynamic Loss for a Turbine Blade With Endwall Leakage Features and Contouring
inferred← citeshttps://doi.org/10.1115/gt2013-95639openalex-snapshot
Experimental and CFD Studies of NGV Endwall Cooling
inferred← citeshttps://doi.org/10.1115/gt2016-56318openalex-snapshot
Turbine Vane Endwall Film Cooling With Slashface Leakage and Discrete Hole Configuration
inferred← citeshttps://doi.org/10.1115/gt2018-77167openalex-snapshot
Meander-Like Shape Optimization of the Stator-Rotor Platform Cavity
inferred← citeshttps://doi.org/10.1115/imece2005-83032openalex-snapshot
Flow Measurements in a First Stage Nozzle Cascade Having Leakage and Assembly Features: Effects of Endwall Steps and Leakage on Aerodynamic Losses
inferred← citeshttps://doi.org/10.1115/imece2006-15092openalex-snapshot
Film Cooling Effectiveness Distributions on a Turbine Blade Cascade Platform With Stator-Rotor Purge and Discrete Film Hole Flows
inferred← citeshttps://doi.org/10.1134/1.1505545openalex-snapshot
A decrease in the effective cross section of a cooling stream caused by hot air penetration into the blowout channel
inferred← citeshttps://doi.org/10.1155/2012/957421openalex-snapshot
Aerodynamic Losses in Turbines with and without Film Cooling, as Influenced by Mainstream Turbulence, Surface Roughness, Airfoil Shape, and Mach Number
inferred← citeshttps://doi.org/10.1155/s1023621x03000149openalex-snapshot
An Experimental Investigation of Transpiration Cooling. Part I: Application of an Infrared Measurement Technique
inferred← citeshttps://doi.org/10.2514/1.16344openalex-snapshot
Turbine Endwall Aerodynamics and Heat Transfer
inferred← citeshttps://doi.org/10.2514/1.30382openalex-snapshot
Effectiveness Distributions on Turbine Blade Cascade Platforms Through Simulated Stator-Rotor Seals
inferred← citeshttps://doi.org/10.2514/5.9781624102660.0275.0310openalex-snapshot
Endwall Aerodynamics and Heat Transfer
inferred← citeshttps://doi.org/10.2514/6.2008-4298openalex-snapshot
Aerothermal Aspects of a Pulsated Inclined Film Cooling Jet in Crossflow
inferred← citeshttps://doi.org/10.2514/6.2011-631openalex-snapshot
Numerical and Experimental Study of Film Cooling Effectiveness and Total Pressure Loss for a Realistic Cascade with an Annular Endwall
inferred← citeshttps://doi.org/10.2514/6.2015-2814openalex-snapshot
Numerical Analysis of Film Cooling Characteristic on a Turbine Non-axisymmetric Contoured Endwall
inferred← citeshttps://doi.org/10.38036/jgpp.5.1_23openalex-snapshot
Development of an Unsteady Multi-Species Numerical Method for Internal Compressible Flows in the Turbine
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