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Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall

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What this work says

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

inferredcites →https://doi.org/10.1016/0142-727x(87)90001-4openalex-snapshot

The generation of nearly isotropic turbulence by means of grids

inferredcites →https://doi.org/10.1016/0894-1777(88)90043-xopenalex-snapshot

Describing the uncertainties in experimental results

inferredcites →https://doi.org/10.1016/j.applthermaleng.2016.01.056openalex-snapshot

Influence of mainstream turbulence on turbine blade platform cooling from simulated swirl purge flow

inferredcites →https://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

inferredcites →https://doi.org/10.1016/j.ast.2020.105923openalex-snapshot

Effects of compound angle on film cooling effectiveness considering endwall lateral pressure gradient

inferredcites →https://doi.org/10.1016/j.ast.2022.107795openalex-snapshot

Trajectory and effectiveness of film cooling in endwall crossflow

inferredcites →https://doi.org/10.1016/j.ijheatmasstransfer.2012.04.024openalex-snapshot

Influence of flow injection angle on a leading-edge horseshoe vortex

inferredcites →https://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

inferredcites →https://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

inferredcites →https://doi.org/10.1016/j.ijthermalsci.2021.107140openalex-snapshot

Effect of leakage flow on the endwall cooling performance in high subsonic turbine cascade

inferredcites →https://doi.org/10.1016/j.ijthermalsci.2022.107821openalex-snapshot

Experimental study of film cooling characteristics of annular cascade endwall with a partitioned film cooling layout

inferredcites →https://doi.org/10.1115/1.2720484openalex-snapshot

Experimental Investigation of Turbine Leakage Flows on the Three-Dimensional Flow Field and Endwall Heat Transfer

inferredcites →https://doi.org/10.1115/1.2813001openalex-snapshot

Boundary Layer Influence on the Unsteady Horseshoe Vortex Flow and Surface Heat Transfer

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/10.1115/1.2841006openalex-snapshot

Flow Visualization in a Linear Turbine Cascade of High Performance Turbine Blades

inferredcites →https://doi.org/10.1115/1.2841353openalex-snapshot

Closure to “Discussion of ‘Heat Transfer and Flowfield Measurements in the Leading Edge Region of a Stator Vane Endwall’” (1999, ASME J. Turbomach., 121, p. 568)

inferredcites →https://doi.org/10.1115/1.3230352openalex-snapshot

Crossflows in a Turbine Cascade Passage

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/10.1115/1.4001135openalex-snapshot

Computational Study of a Midpassage Gap and Upstream Slot on Vane Endwall Film-Cooling

inferredcites →https://doi.org/10.1115/1.4002965openalex-snapshot

Effects of an Axisymmetric Contoured Endwall on a Nozzle Guide Vane: Adiabatic Effectiveness Measurements

inferredcites →https://doi.org/10.1115/1.4045876openalex-snapshot

Turbine Vane Endwall Film Cooling Effectiveness of Different Purge Slot Configurations in a Linear Cascade

inferredcites →https://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

inferredcites →https://doi.org/10.1115/1.4050357openalex-snapshot

Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade

inferredcites →https://doi.org/10.1115/1.4050566openalex-snapshot

An Experimental Study of the Leakage Flow Effect on the Film Cooling Effectiveness of a Gas Turbine Shroud

inferredcites →https://doi.org/10.1115/1.4052456openalex-snapshot

Comparison of Film Cooling Performance for Different Purge Slot Configurations in a Cylindrical and State-of-the-Art Nozzle Guide Vane

inferredcites →https://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

inferredcites →https://doi.org/10.2514/1.b36640openalex-snapshot

Effects of Upstream Endwall Film Cooling on a Vane Cascade Flowfield

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.4646853openalex-extracted

Effect of Misalignment and Turbulence Level on Film Cooling Characteristic of a Turbine Concave Endwall with Upstream Leakage Flow

inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2024.122671openalex-snapshot

Effect of backward-facing step and turbulence level on film cooling characteristic of a turbine concave endwall with upstream leakage flow

inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2024.124423openalex-snapshot

Experimental and numerical study on integrated film cooling of turbine endwall by upstream slot leakage and blade showerhead jets

inferred← citeshttps://doi.org/10.1016/j.ijheatfluidflow.2026.110345openalex-snapshot

Cooling scheme from phantom cooling effect using vane film coolant on the endwall surface

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.2026.111102openalex-snapshot

Unsteady ingestion and jet film cooling characteristics of multi-gap turbine endwall under periodic upstream wake passing

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/10.1115/1.4066272openalex-snapshot

Aerothermal Performance of Slashface Leakage With Double Surface Angle Under Realistic Swirling Inflow

inferred← citeshttps://doi.org/10.1177/09576509251331255openalex-snapshot

High–pressure turbine rotor blade end-wall flow and cooling characteristics: Trends and perspectives

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