On the public citation graph

Adiabatic and Overall Effectiveness for a Fully Cooled Turbine Vane

https://doi.org/10.1115/gt2013-94928
0 signed · 34 inferred · view as graph

Inferred edges come from two machine sources: sweeps of open repository metadata (mostly SSRN and Zenodo), and a bulk OpenAlex citation snapshot. Every row below is labelled with the one it came from. Neither is a complete citation index — absence here is not evidence of absence.

Is this your work? Sign in with ORCID and put your name on the claims that are yours.
Claim with ORCID
Reference health. See whether every reference in this work resolves to a known work and none has been retracted — and get a dated CiteStamped badge you can embed.
See reference health

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.4066399openalex-extracted
Mini-Channel Embedded Film Cooled Flat Plate
inferred← citeshttps://doi.org/10.2139/ssrn.4493702openalex-extracted
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2023.121466openalex-snapshot
An experimental and numerical study on the blade tip conjugate heat transfer performance
inferred← citeshttps://doi.org/10.1016/j.applthermaleng.2024.122662openalex-snapshot
Investigation on the effect of hole diameter and wall thickness on the overall cooling effectiveness of turbine vane leading edge
inferred← citeshttps://doi.org/10.1016/j.expthermflusci.2016.12.008openalex-snapshot
Conjugate heat transfer on full-coverage film cooling with array jet impingements with various Biot numbers
inferred← citeshttps://doi.org/10.1016/j.icheatmasstransfer.2026.111448openalex-snapshot
Effect of anisotropic thermal conductivity on cooling performance of a film cooled CMC turbine vane
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2021.121377openalex-snapshot
Experimental study on film cooling and heat transfer characteristics of a twisted vane with staggered counter-inclined film-hole and laid-back-shaped-hole
inferred← citeshttps://doi.org/10.1016/j.ijheatmasstransfer.2026.129282openalex-snapshot
Estimation of internal and external heat loads by inverse conduction analysis of internally-cooled turbine vane
inferred← citeshttps://doi.org/10.1016/j.tsep.2023.102261openalex-snapshot
Experimental investigation of full-coverage film cooling characteristic of single/double-wall cooling vane
inferred← citeshttps://doi.org/10.1108/hff-03-2023-0157openalex-snapshot
Mini-channel embedded film cooled flat plate: conjugate heat transfer analysis and enhancement study
inferred← citeshttps://doi.org/10.1115/1.4032456openalex-snapshot
The Delta Phi Method of Evaluating Overall Film Cooling Performance
inferred← citeshttps://doi.org/10.1115/1.4036200openalex-snapshot
Experimentally Measured Effects of Incidence Angle on the Adiabatic and Overall Effectiveness of a Fully Cooled Turbine Airfoil With Shaped Showerhead Holes
inferred← citeshttps://doi.org/10.1115/1.4037997openalex-snapshot
Effect of Internal Crossflow Velocity on Film Cooling Effectiveness—Part I: Axial Shaped Holes
inferred← citeshttps://doi.org/10.1115/1.4037998openalex-snapshot
Effect of Internal Crossflow Velocity on Film Cooling Effectiveness—Part II: Compound Angle Shaped Holes
inferred← citeshttps://doi.org/10.1115/1.4041292openalex-snapshot
Influence of Scaling Parameters and Gas Properties on Overall Effectiveness on a Leading Edge Showerhead
inferred← citeshttps://doi.org/10.1115/1.4041645openalex-snapshot
Experimental Evaluations of the Relative Contributions to Overall Effectiveness in Turbine Blade Leading Edge Cooling
inferred← citeshttps://doi.org/10.1115/1.4045875openalex-snapshot
A Parametric Investigation of Vane Showerhead Film Cooling by Pressure-Sensitive Paint Technique
inferred← citeshttps://doi.org/10.1115/1.4045987openalex-snapshot
A Computational Technique to Evaluate the Relative Influence of Internal and External Cooling on Overall Effectiveness
inferred← citeshttps://doi.org/10.1115/1.4051073openalex-snapshot
Heat Transfer Characteristics Analysis on a Fully Cooled Vane With Varied Density Ratios
inferred← citeshttps://doi.org/10.1115/1.4056390openalex-snapshot
Evaluation of Adjoint-Optimized Holes—Part I Baseline Performance
inferred← citeshttps://doi.org/10.1115/1.4062279openalex-snapshot
Impact of Temperature Ratio on Overall Cooling Performance: Low-Order-Model-Based Analysis of Experiment Design
inferred← citeshttps://doi.org/10.1115/1.4062436openalex-snapshot
Film Cooling Comparison of Full-Scale Turbine Vanes Using the Pressure Sensitive Paint Technique
inferred← citeshttps://doi.org/10.1115/1.4063927openalex-snapshot
The Effects of Channel Supplies on Overall Film-Cooling Effectiveness
inferred← citeshttps://doi.org/10.1115/1.4068460openalex-snapshot
Impact of Temperature Ratio on Overall Cooling Effectiveness: Experimental Validation of a Scaling Theory
inferred← citeshttps://doi.org/10.1115/1.4069762openalex-snapshot
Simplified Model and Approach to Transform Infrared Surface Temperature to Film Effectiveness in a Conjugate Heat Transfer Experiment
inferred← citeshttps://doi.org/10.1115/1.4069813openalex-snapshot
Comparative Investigation of HPT Blade Cooling Concepts in an Aerothermal Test Rig
inferred← citeshttps://doi.org/10.1115/gt2016-57982openalex-snapshot
Experimentally Measured Effects of Incidence Angle on the Adiabatic and Overall Effectiveness of a Fully Cooled Turbine Airfoil With Showerhead Shaped Holes
inferred← citeshttps://doi.org/10.1115/gt2017-64616openalex-snapshot
Effect of Internal Crossflow Velocity on Film Cooling Effectiveness: Part I — Axial Shaped Holes
inferred← citeshttps://doi.org/10.1115/gt2017-64624openalex-snapshot
Effect of Internal Crossflow Velocity on Film Cooling Effectiveness: Part II — Compound Angle Shaped Holes
inferred← citeshttps://doi.org/10.1115/gt2018-75332openalex-snapshot
Influence of Scaling Parameters and Gas Properties on Overall Effectiveness on a Leading Edge Showerhead
inferred← citeshttps://doi.org/10.1115/gt2018-75334openalex-snapshot
Experimental Evaluations of the Relative Contributions to Overall Effectiveness in Turbine Blade Leading Edge Cooling
inferred← citeshttps://doi.org/10.1115/gt2019-90999openalex-snapshot
A Computational Technique to Evaluate the Relative Influence of Internal and External Cooling on Overall Effectiveness
inferred← citeshttps://doi.org/10.1615/heattransres.2025056820openalex-snapshot
ASSESSMENT OF SHAPED FILM HOLES UNDER CONJUGATE HEAT TRANSFER CONDITIONS
inferred← citeshttps://doi.org/10.31026/j.eng.2016.06.08openalex-snapshot
The Effects of Inclination and Compounds Angles of Round Holes in Staggered Rows on Adiabatic Film Cooling Effectiveness of Vane Suction side
Editorial review for independent work. ICSAC — the Institute for Complexity Science and Advanced Computing — runs a structured editorial panel for researchers publishing outside journals, and publishes on CiteStamp rails. Submission is free and goes through ORCID: icsacinstitute.org/submit.