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Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint

https://doi.org/10.1115/1.1400113
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What this work says

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

inferredcites →https://doi.org/10.1115/1.2836637openalex-snapshot
Film Cooling of the Gas Turbine Endwall by Discrete-Hole Injection
inferredcites →https://doi.org/10.1115/1.2836731openalex-snapshot
The Design of an Improved Endwall Film-Cooling Configuration
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/10.1115/1.2841189openalex-snapshot
Aerodynamic Aspects of Endwall Film-Cooling
inferredcites →https://doi.org/10.1115/1.2927684openalex-snapshot
An Experimental Study of Heat Transfer and Film Cooling on Low Aspect Ratio Turbine Nozzles
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/10.1115/2000-gt-0214openalex-snapshot
Measurements in a Turbine Cascade Over a Contoured Endwall: Discrete Hole Injection of Bleed Flow
inferredcites →https://doi.org/10.1115/2000-gt-0247openalex-snapshot
The Effects of Injection Angle and Hole Exit Shape on Turbine Nozzle Pressure Side Film Cooling
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/10.1115/91-gt-253openalex-snapshot
Film Cooling Research on the Endwall of a Turbine Nozzle Guide Vane in a Short Duration Annular Cascade: Part 2 — Analysis and Correlation of Results
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/10.1115/96-gt-208openalex-snapshot
Aerodynamic Aspects of Endwall Film-Cooling
inferredcites →https://doi.org/10.1115/96-gt-255openalex-snapshot
Experimental Contribution on the Significance and the Control by Transverse Injection of the Horseshoe Vortex
inferredcites →https://doi.org/10.1115/98-gt-483openalex-snapshot
The Design of an Improved Endwall Film-Cooling Configuration
inferredcites →https://doi.org/10.1115/99-gt-196openalex-snapshot
Turbine Nozzle Film Cooling Study Using the Pressure Sensitive Paint (PSP) Technique

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/10.1007/978-3-030-68056-5_11openalex-snapshot
Extended Applications of PSP and TSP
inferred← citeshttps://doi.org/10.1007/s11630-025-2026-4openalex-snapshot
Experimental and Numerical Investigation on Cooling and Aerodynamic Performance of Turbine Blade Ribbed Squealer Tip
inferred← citeshttps://doi.org/10.1007/s11630-025-2210-6openalex-snapshot
Film-Cooling Effectiveness Investigation of Various Diffusion Slot Hole Geometries on Turbine Guide Vane Endwall
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2016.07.019openalex-snapshot
Effects of wall curvature and streamwise pressure gradient on film cooling effectiveness
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2019.114851openalex-snapshot
Experimental investigation of film cooling effectiveness on a gas turbine blade pressure surface with diffusion slot holes
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2020.116126openalex-snapshot
Study of an effusion-cooled plate with high level of upstream fluctuation
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2023.121862openalex-snapshot
A comprehensive deviation analysis of film cooling effectiveness measurements using pressure sensitive paint under various conditions
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.applthermaleng.2026.129883openalex-snapshot
Experimental study on suction side film cooling characteristics of an adjustable turbine guide vane under different turning angles for a variable cycle engine
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2026.130194openalex-snapshot
Film-cooling effectiveness experiments on turbine rotor blade leading edge with various diffusion slot hole geometries and layouts
inferred← citeshttps://doi.org/10.1016/j.ast.2023.108658openalex-snapshot
Experimental and numerical investigations of vane endwall film cooling with different cooling hole configurations
inferred← citeshttps://doi.org/10.1016/j.cja.2018.03.008openalex-snapshot
Effect of inlet rotating swirl on endwall film cooling for two representative hole arrangements
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.2015.08.002openalex-snapshot
An experimental investigation of geometric effect of upstream converging slot-hole on end-wall film cooling and secondary vortex characteristics
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.expthermflusci.2024.111267openalex-snapshot
Experimental investigation on seeping gas film effectiveness in supersonic flow downstream of a porous injector
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2021.105132openalex-snapshot
An innovative design for measuring the enhanced mixing effect of a shock wave on supersonic film cooling
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2023.106778openalex-snapshot
Experimental and numerical investigations of vane endwall film cooling with different density ratios
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2025.110414openalex-snapshot
Investigation of swirl-induced film cooling deterioration and mechanism-based layout optimization for pressure side in variable geometry turbines
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.2006.06.028openalex-snapshot
Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2012.03.064openalex-snapshot
Multi-parameter influence on combined-hole film cooling system
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2013.06.065openalex-snapshot
Film cooling effectiveness distribution on first-stage vane endwall with and without leading-edge fillets
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2014.04.028openalex-snapshot
An experimental study of density ratio effects on the film cooling injection from discrete holes by using PIV and PSP techniques
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2014.11.067openalex-snapshot
Film cooling effectiveness in the region of the blade-endwall corner junction with the injection assisted by the recirculating vortex flow
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2015.03.017openalex-snapshot
Effects of compound angle on film cooling effectiveness with different streamwise pressure gradient and convex curvature
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.2015.08.049openalex-snapshot
Multi-row film cooling characteristics on a 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.2016.07.028openalex-snapshot
Film cooling effectiveness measurements of a near surface streamwise diffusion hole
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2017.08.077openalex-snapshot
Film cooling effectiveness for three-row compound angle hole design on flat plate using PSP technique
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2018.11.153openalex-snapshot
Effect of gas turbine endwall misalignment with slashface leakage on the blade endwall aerothermal performance
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.2019.05.109openalex-snapshot
Turbine platform phantom cooling from airfoil film coolant, with purge flow
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2020.120565openalex-snapshot
Film Cooling Patterns over an Aircraft Engine Turbine Endwall with Slot Leakage and Discrete Hole Injection
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2021.107434openalex-snapshot
Experimental evaluation of cooling effectiveness from novel film holes over turbine endwalls with inlet swirl
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2022.107482openalex-snapshot
Numerical analysis of vane endwall film cooling and heat transfer with different mainstream turbulence intensities and blowing ratios
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2024.109440openalex-snapshot
Experimental study on endwall film cooling performance of an adjustable guide vane
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2025.109786openalex-snapshot
Theoretical study on showerhead film cooling effectiveness of adjustable guide vane installation angle for variable cycle Aeroengine
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/10.1063/1.5110726openalex-snapshot
Performance analysis of different influencing factors on film cooling and the internal relations with vortex structures
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/10.1080/01457632.2026.2649999openalex-snapshot
Enhanced Thermal Performance of Aircraft Gas Turbine Blades Using Bio-Inspired Microstructured Surfaces
inferred← citeshttps://doi.org/10.1108/hff-12-2020-0804openalex-snapshot
Numerical investigations of endwall film cooling design of a turbine vane using four-holes pattern
inferred← citeshttps://doi.org/10.1115/1.1561811openalex-snapshot
Combustor Turbine Interface Studies—Part 1: Endwall Effectiveness Measurements
inferred← citeshttps://doi.org/10.1115/1.1909208openalex-snapshot
Film-Cooling Effectiveness on a Gas Turbine Blade Tip Using Pressure-Sensitive Paint
inferred← citeshttps://doi.org/10.1115/1.1929809openalex-snapshot
Adiabatic Effectiveness Measurements and Predictions of Leakage Flows Along a Blade Endwall
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/10.1115/1.2241945openalex-snapshot
Film Cooling Effectiveness on the Leading Edge Region of a Rotating Turbine Blade With Two Rows of Film Cooling Holes Using Pressure Sensitive Paint
inferred← citeshttps://doi.org/10.1115/1.2464142openalex-snapshot
Gas Turbine Heat Transfer: Ten Remaining Hot Gas Path Challenges
inferred← citeshttps://doi.org/10.1115/1.2720493openalex-snapshot
A Comparison of Cylindrical and Fan-Shaped Film-Cooling Holes on a Vane Endwall at Low and High Freestream Turbulence Levels
inferred← citeshttps://doi.org/10.1115/1.2720497openalex-snapshot
The Effects of Varying the Combustor-Turbine Gap
inferred← citeshttps://doi.org/10.1115/1.2720506openalex-snapshot
Heat Transfer Measurements in a First-Stage Nozzle Cascade Having Endwall Contouring: Misalignment and Leakage Studies
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/10.1115/1.2907440openalex-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/10.1115/1.3068327openalex-snapshot
Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling
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/10.1115/1.4001135openalex-snapshot
Computational Study of a Midpassage Gap and Upstream Slot on Vane Endwall Film-Cooling
inferred← citeshttps://doi.org/10.1115/1.4002422openalex-snapshot
Effect of Upstream Step on Flat Plate Film-Cooling Effectiveness Using PSP
inferred← citeshttps://doi.org/10.1115/1.4002988openalex-snapshot
Effect of Density Ratio on Flat Plate Film Cooling With Shaped Holes Using PSP
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/10.1115/1.4003725openalex-snapshot
Film Cooling Effect of Rotor-Stator Purge Flow on Endwall Heat/Mass Transfer
inferred← citeshttps://doi.org/10.1115/1.4005732openalex-snapshot
Influence of Coolant Density on Turbine Blade Platform Film-Cooling
inferred← citeshttps://doi.org/10.1115/1.4007879openalex-snapshot
Film Cooling of Cylindrical Hole With a Downstream Short Crescent-Shaped Block
inferred← citeshttps://doi.org/10.1115/1.4023826openalex-snapshot
Fundamental Gas Turbine Heat Transfer
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/10.1115/1.4026964openalex-snapshot
Influence of Coolant Density on Turbine Platform Film-Cooling With Stator–Rotor Purge Flow and Compound-Angle Holes
inferred← citeshttps://doi.org/10.1115/1.4032883openalex-snapshot
Geometrical Optimization and Experimental Validation of a Tripod Film Cooling Hole With Asymmetric Side Holes
inferred← citeshttps://doi.org/10.1115/1.4033506openalex-snapshot
Measurement Uncertainty Analysis in Determining Adiabatic Film Cooling Effectiveness by Using Pressure Sensitive Paint Technique
inferred← citeshttps://doi.org/10.1115/1.4034985openalex-snapshot
Turbine Blade Platform Film Cooling With Simulated Swirl Purge Flow and Slashface Leakage Conditions
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/10.1115/1.4036007openalex-snapshot
Geometrical Parameter Effects on Film-Cooling Effectiveness of Rectangular Diffusion Holes
inferred← citeshttps://doi.org/10.1115/1.4038150openalex-snapshot
Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions
inferred← citeshttps://doi.org/10.1115/1.4039644openalex-snapshot
Advanced Cooling in Gas Turbines 2016 Max Jakob Memorial Award Paper
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/10.1115/1.4042057openalex-snapshot
Turbine Vane Endwall Film Cooling Comparison From Five Film-Hole Design Patterns and Three Upstream Injection Angles
inferred← citeshttps://doi.org/10.1115/1.4044806openalex-snapshot
Effects of Mainstream Turbulence Intensity and Coolant-to-Mainstream Density Ratio on Film Cooling Effectiveness of Multirow Diffusion Slot Holes
inferred← citeshttps://doi.org/10.1115/1.4045069openalex-snapshot
Design of Full-Scale Endwall Film Cooling of a Turbine Vane
inferred← citeshttps://doi.org/10.1115/1.4047284openalex-snapshot
A Novel Single-Passage Transonic Wind Tunnel for Turbine-Vane Film Cooling
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/10.1115/1.4052457openalex-snapshot
Endwall Heat Transfer and Cooling Performance of a Transonic Turbine Vane With Upstream Injection Flow
inferred← citeshttps://doi.org/10.1115/1.4052500openalex-snapshot
The Effects of Axisymmetric Convergent Contouring and Blowing Ratio on Endwall Film Cooling and Vane Pressure Side Surface Phantom Cooling Performance
inferred← citeshttps://doi.org/10.1115/1.4052754openalex-snapshot
Experimental Study of the Endwall Heat Transfer of a Transonic Nozzle Guide Vane With Upstream Jet Purge Cooling Part 1—Effect of Density Ratio
inferred← citeshttps://doi.org/10.1115/1.4053915openalex-snapshot
Effect of Coolant Crossflow on Film Cooling Effectiveness of Diffusion Slot Hole With and Without Ribs
inferred← citeshttps://doi.org/10.1115/1.4054525openalex-snapshot
Experimental and Numerical Investigations Into the Blade Tip Phantom Cooling Performance
inferred← citeshttps://doi.org/10.1115/1.4054543openalex-snapshot
Detached Eddy Simulation of the Unsteady Flow and Film Cooling Characteristics of an Endwall With an Interrupted Slot
inferred← citeshttps://doi.org/10.1115/1.4055268openalex-snapshot
Sensitivity of Adiabatic Cooling Effectiveness to Mainstream and Coolant Temperatures in Transonic Flow Over an Idealized Blade Tip Model
inferred← citeshttps://doi.org/10.1115/1.4062180openalex-snapshot
Upstream Jet Cooling and Dual Cavity Slashface Leakage Cooling on a Transonic Nozzle Guide Vane Endwall
inferred← citeshttps://doi.org/10.1115/1.4062805openalex-snapshot
Film Cooling Effectiveness on Pressure Surface and Suction Surface of Turbine Guide Vane With Diffusion Slot Holes
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/10.1115/1.4063922openalex-snapshot
Study on Additive Effect of Film Cooling Effectiveness in Two Rows of Fan-Shaped Holes
inferred← citeshttps://doi.org/10.1115/1.4064429openalex-snapshot
Improving Turbine Endwall Overall Cooling Effectiveness Using Curtain Cooling and Redistributed Film-Hole Layouts: An Experimental and Computational Study
inferred← citeshttps://doi.org/10.1115/1.4068907openalex-snapshot
Effects of Upstream Step Geometries on the Turbine Endwall Aerothermal Performance With Fan-Shaped Holes
inferred← citeshttps://doi.org/10.1115/gt2006-91067openalex-snapshot
Computational Study of a Midpassage Gap and Upstream Slot on Vane Endwall Film-Cooling
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/gt2014-25212openalex-snapshot
Optimization of the Hole Exit Shaping of Film Holes Without and With Compound Angles for Maximal Film Cooling Effectiveness
inferred← citeshttps://doi.org/10.1115/gt2014-26232openalex-snapshot
Film Cooling With Forward and Backward Injection for Cylindrical and Fan-Shaped Holes Using PSP Measurement Technique
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/gt2016-56321openalex-snapshot
Turbine Blade Platform Film Cooling With Simulated Swirl Purge Flow and Slashface Leakage Conditions
inferred← citeshttps://doi.org/10.1115/gt2017-63119openalex-snapshot
Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions
inferred← citeshttps://doi.org/10.1115/gt2020-14814openalex-snapshot
Experimental Study of the Endwall Heat Transfer of a Transonic Nozzle Guide Vane With Upstream Jet Purge Cooling: Part 1 — Effect of Density Ratio
inferred← citeshttps://doi.org/10.1115/gt2020-16160openalex-snapshot
Endwall Heat Transfer and Cooling Performance of a Transonic Turbine Vane With Upstream Injection Flow
inferred← citeshttps://doi.org/10.1115/imece2005-80146openalex-snapshot
Assessment of Steady State PSP and Transient Ir Measurement Techniques for Leading Edge Film Cooling
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/10.1177/0954410016673092openalex-snapshot
Improving turbine endwall cooling uniformity by controlling near-wall secondary flows
inferred← citeshttps://doi.org/10.1177/09576509251331255openalex-snapshot
High–pressure turbine rotor blade end-wall flow and cooling characteristics: Trends and perspectives
inferred← citeshttps://doi.org/10.1515/tjj-2024-0008openalex-snapshot
The overall film cooling performance of crescent holes
inferred← citeshttps://doi.org/10.2139/ssrn.4806113openalex-snapshot
Experimental Investigation on Seeping Gas Film Effectiveness in Supersonic Flow Downstream Porous Injector
inferred← citeshttps://doi.org/10.2514/1.16344openalex-snapshot
Turbine Endwall Aerodynamics and Heat Transfer
inferred← citeshttps://doi.org/10.2514/1.19201openalex-snapshot
Film-Cooling Effectiveness on Squealer Cavity and Rim Walls of Gas-Turbine Blade Tip
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/10.2514/1.42411openalex-snapshot
Upstream Vortex Effects on Turbine Blade Platform Film Cooling With Typical Purge Flow
inferred← citeshttps://doi.org/10.2514/1.54202openalex-snapshot
Study of Trailing-Edge Cooling Using Pressure Sensitive Paint Technique
inferred← citeshttps://doi.org/10.2514/1.j054191openalex-snapshot
Measuring Surface Pressures on Rotor Blades Using Pressure-Sensitive Paint
inferred← citeshttps://doi.org/10.2514/1.t5339openalex-snapshot
Combustor Wall Coolant Discharge Effects on Turbine Vane Endwall Curtain Cooling
inferred← citeshttps://doi.org/10.2514/1.t6607openalex-snapshot
Upstream Endwall Film-Cooing in a Vane Cascade with Cylindrical Shape Holes
inferred← citeshttps://doi.org/10.2514/5.9781624102660.0275.0310openalex-snapshot
Endwall Aerodynamics and Heat Transfer
inferred← citeshttps://doi.org/10.2514/6.2006-3402openalex-snapshot
Effectiveness Distributions on Turbine Blade Cascade Platforms through Simulated Stator-Rotor Seals
inferred← citeshttps://doi.org/10.2514/6.2010-405openalex-snapshot
Numerical and Experimental Study of Trenched Film Hole Cooling for a Realistic Cascade in an Annular Endwall, Phase1: Test Rig Construction and Preliminary Data
inferred← citeshttps://doi.org/10.2514/6.2011-3269openalex-snapshot
An Experimental Investigation on the Trailing Edge Cooling of Turbine Blades by using PIV and PSP Techniques
inferred← citeshttps://doi.org/10.2514/6.2017-4826openalex-snapshot
Influence of Discharge from Combustor Walls on Curtain Cooling for a First-Stage Turbine Vane Endwall
inferred← citeshttps://doi.org/10.33737/gpps21-tc-116openalex-snapshot
Influence of Combustor Exit Conditions on Cooling Performance of NGV Endwall with Double Row Cooling Holes
inferred← citeshttps://doi.org/10.3390/aerospace10080702openalex-snapshot
Recent Developments in the Aerodynamic Heat Transfer and Cooling Technology of Gas Turbines Endwalls
inferred← citeshttps://doi.org/10.3390/aerospace12060533openalex-snapshot
Film Cooling Performance and Superposition Method of an Actual Turbine Vane at High Freestream Turbulence
inferred← citeshttps://doi.org/10.3390/en15196968openalex-snapshot
Review of Film Cooling in Gas Turbines with an Emphasis on Additive Manufacturing-Based Design Evolutions
inferred← citeshttps://doi.org/10.3390/en16237733openalex-snapshot
Experimental Study on the Improvement of Film Cooling Effectiveness of Various Modified Configurations Based on a Fan-Shaped Film Cooling Hole on an Endwall
inferred← citeshttps://doi.org/10.3390/en16237752openalex-snapshot
Experimental Study on the Improvement of the Film Cooling Effectiveness of Various Modified Configurations Based on a Fan-Shaped Film Cooling Hole on a Flat Plate
inferred← citeshttps://doi.org/10.3390/pr10112335openalex-snapshot
Data-Driven Conjugate Heat Transfer Analysis of a Gas Turbine Vane
inferred← citeshttps://doi.org/10.4028/www.scientific.net/ddf.379.83openalex-snapshot
A Deep Insight to Secondary Flows
inferred← citeshttps://doi.org/10.5098/hmt.v1.1.3001openalex-snapshot
TURBINE BLADE FILM COOLING USING PSP TECHNIQUE
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