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Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II—Heat Transfer and Film-Cooling Effectiveness
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What this work says
Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1007/978-3-662-10037-0_2openalex-snapshot
Einführung in die Statistik
inferredcites →https://doi.org/10.1007/bf01589919openalex-snapshot
Similarity analysis of model experiments for film cooling in gas turbines
inferredcites →https://doi.org/10.1115/1.2836637openalex-snapshot
Film Cooling of the Gas Turbine Endwall by Discrete-Hole Injection
inferredcites →https://doi.org/10.1115/1.2840916openalex-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/10.1115/1.2927684openalex-snapshot
An Experimental Study of Heat Transfer and Film Cooling on Low Aspect Ratio Turbine Nozzles
inferredcites →https://doi.org/10.1115/1.2927693openalex-snapshot
Experimental Determination of Stator Endwall Heat Transfer
inferredcites →https://doi.org/10.1115/1.2927900openalex-snapshot
Film Cooling in the Presence of Mainstream Pressure Gradients
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/10.1115/1.3239529openalex-snapshot
An Experimental Investigation of Endwall Heat Transfer and Aerodynamics in a Linear Vane Cascade
inferredcites →https://doi.org/10.1115/1.3239530openalex-snapshot
Comparison of Visualized Turbine Endwall Secondary Flows and Measured Heat Transfer Patterns
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/10.1115/1.3262234openalex-snapshot
Aerodynamic and Heat Transfer Measurements on a Transonic Nozzle Guide Vane
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/10.1115/1.3609155openalex-snapshot
Heat Transfer With Film Cooling Near Nontangential Injection Slots
inferredcites →https://doi.org/10.1115/2000-gt-0200openalex-snapshot
Effects of Slot Bleed Injection Over a Contoured End Wall on Nozzle Guide Vane Cooling Performance: Part II — Thermal 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
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
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Numerical Study on the Effect of Rim Seal Slot Filleting on Turbine Endwall Cooling Performance
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3D Measurements of coupled freestream turbulence and secondary flow effects on film cooling
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Effects of Trenched Film Hole Configurations on the Endwall Film Cooling and Suction Side Phantom Cooling
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Improved Turbine Vane Endwall Film Cooling by Using Sand-Dune-Inspired Design
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Numerical simulation of liquid film and regenerative cooling in a liquid rocket
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Effect of discrete-hole arrangement on film-cooling effectiveness for the endwall of a turbine blade cascade
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Influence of the upstream slot geometry on the endwall cooling and phantom cooling of vane suction side surface
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Effect of the wake on the heat transfer of a turbine blade endwall according to relative position of the cylindrical rod
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Endwall film cooling performance considering the effects of micro-riblets configurations and layouts
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Numerical analysis of multiple influences on turbine vane endwall film cooling characteristics
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Heat transfer and film-cooling for the endwall of a first stage turbine vane
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Influence of flow injection angle on a leading-edge horseshoe vortex
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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.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.2016.07.033openalex-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.2017.05.010openalex-snapshot
Effects of the mainstream turbulence intensity and slot injection angle on the endwall cooling and phantom cooling of the vane suction side surface
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Effects of the swirling coolant jet from the upstream slot on the vane endwall cooling and the vane suction side phantom cooling
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
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Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection
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Influence of endwall 2D contouring on endwall adiabatic cooling effectiveness and aerodynamic performance
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Turbine platform phantom cooling from airfoil film coolant, with purge flow
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Conjugate heat transfer measurements and predictions for the vane endwall of a high-pressure turbine with upstream purge flow
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Turbine vane endwall partition film cooling based on the passage vortex core line
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Film Cooling Patterns over an Aircraft Engine Turbine Endwall with Slot Leakage and Discrete Hole Injection
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.ijheatmasstransfer.2024.125403openalex-snapshot
Non-axisymmetric Endwall film cooling characteristics considering the influences of cylindrical holes and laidback fan-shaped holes
inferred← citeshttps://doi.org/10.1016/j.ijthermalsci.2020.106562openalex-snapshot
Full coverage film cooling on a non-axisymmetric contoured endwall and the baseline endwall
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/s0017-9310(02)00529-xopenalex-snapshot
Heat transfer––a review of 2001 literature
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/10.1063/5.0270875openalex-snapshot
Genetic algorithm-based optimal film cooling design for gas turbine endwalls under real operating conditions
inferred← citeshttps://doi.org/10.1080/08916152.2021.1933651openalex-snapshot
Heat transfer measurements of a turbine endwall with engine-representative freestream turbulence and inlet swirl
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/10.1115/1.1561811openalex-snapshot
Combustor Turbine Interface Studies—Part 1: Endwall Effectiveness Measurements
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/10.1115/1.2098791openalex-snapshot
Effect of Midpassage Gap, Endwall Misalignment, and Roughness on Endwall Film-Cooling
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The Effects of Varying the Combustor-Turbine Gap
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Film-Cooling Effectiveness on a Rotating Blade Platform
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Film Cooling Effectiveness Distributions on a Turbine Blade Cascade Platform With Stator-Rotor Purge and Discrete Film Hole Flows
inferred← citeshttps://doi.org/10.1115/1.2812950openalex-snapshot
The Effect of Combustor-Turbine Interface Gap Leakage on the Endwall Heat Transfer for a Nozzle Guide Vane
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
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Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling
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Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique
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Computational Study of a Midpassage Gap and Upstream Slot on Vane Endwall Film-Cooling
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Modeling of Heat Transfer in Microchannel Gas Flow
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Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane: Convective Heat Transfer Measurements
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Aerodynamic and Endwall Film-Cooling Investigations of a Gas Turbine Nozzle Guide Vane Applying Temperature-Sensitive Paint
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Effects of Orientation and Position of the Combustor-Turbine Interface on the Cooling of a Vane Endwall
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Influence of Coolant Density on Turbine Blade Platform Film-Cooling
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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
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Leading Edge Shielding Concept in Gas Turbines With Can Combustors
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Influence of Coolant Density on Turbine Platform Film-Cooling With Stator–Rotor Purge Flow and Compound-Angle Holes
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A Novel Transient Technique to Determine Recovery Temperature, Heat Transfer Coefficient, and Film Cooling Effectiveness Simultaneously in a Transonic Turbine Cascade
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Turbine Platform Cooling and Blade Suction Surface Phantom Cooling From Simulated Swirl Purge Flow
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The Combined Effects of an Upstream Ramp and Swirling Coolant Flow on Film Cooling Characteristics
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Turbine Blade Platform Film Cooling With Simulated Swirl Purge Flow and Slashface Leakage Conditions
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Influence of Combustor Swirl on Endwall Heat Transfer and Film Cooling Effectiveness at the Large Scale Turbine Rig
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A Sector-Cascade Test Rig for Measurements of Heat Transfer in Turbine Center Frames
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Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results
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Development of a Modified RANS-Turbulence Model for the Computational Investigation of Film Cooling
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A novel scalar tracking method for optimising film cooling systems
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Turbine Endwall Aerodynamics and Heat Transfer
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Jet-into-Crossflow Boundary-Layer Control: Innovation in Gas Turbine Blade Cooling
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Effectiveness Distributions on Turbine Blade Cascade Platforms Through Simulated Stator-Rotor Seals
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Upstream Vortex Effects on Turbine Blade Platform Film Cooling With Typical Purge Flow
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Numerical Simulation of Liquid Film in a Liquid Oxygen/Rocket Propellant 1 Liquid Rocket
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inferred← citeshttps://doi.org/10.2514/1.t5339openalex-snapshot
Combustor Wall Coolant Discharge Effects on Turbine Vane Endwall Curtain Cooling
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Thermal Management of a Transonic Turbine: Leakage Flow and Endwall Contouring Effects
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Upstream Endwall Film-Cooing in a Vane Cascade with Cylindrical Shape Holes
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Endwall Aerodynamics and Heat Transfer
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Effectiveness Distributions on Turbine Blade Cascade Platforms through Simulated Stator-Rotor Seals
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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/10.2514/6.2011-631openalex-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/10.2514/6.2017-4826openalex-snapshot
Influence of Discharge from Combustor Walls on Curtain Cooling for a First-Stage Turbine Vane Endwall
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Experimental investigation of the influence of density ratio and vane exit mach number on platform cooling
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Effects of Gas Thermophysical Properties on the Full-Range Endwall Film Cooling of a Turbine Vane
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Recent Developments in the Aerodynamic Heat Transfer and Cooling Technology of Gas Turbines Endwalls
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