Research graph
References from Endwall flow patterns and film cooling performance under pulsatile conditions of hydrogen-combustion turbines. Local targets link to admitted publications; unresolved targets remain external evidence.
Unresolved reference
External reference
Review of the impact of hydrogen-containing fuels on gas turbine hot-section materials
10.1115/1.4067335 · 2025 · External reference
Using hydrogen as gas turbine fuel
10.1115/1.1787513 · 2005 · External reference
Flow visualization in a linear turbine cascade of high-performance turbine blades
10.1115/1.2841006 · 1997 · External reference
10.1115/2000-gt-0201
10.1115/2000-gt-0201 · External reference
Effects of an axisymmetric contoured endwall on a nozzle guide vane: convective heat transfer measurements
2011 · External reference
Study of effects of axisymmetric endwall contouring on film cooling/heat transfer and secondary losses in a cascade of first stage nozzle guide vane
2020 · External reference
Influence of endwall 2D contouring on endwall adiabatic cooling effectiveness and aerodynamic performance
10.1016/j.ijheatmasstransfer.2019.02.089 · 2019 · External reference
The effects of axisymmetric convergent contouring and blowing ratio on endwall film cooling and vane pressure side surface phantom cooling performance
10.1115/1.4052500 · 2022 · External reference
Research advances on mist assisted impingement and film cooling of turbine blades
10.1016/j.ijheatmasstransfer.2024.125907 · 2024 · External reference
Review of turbine cooling technologies
2023 · External reference
10.1115/imece2017-72157
10.1115/imece2017-72157 · External reference
Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection
10.1016/j.ijheatmasstransfer.2018.12.079 · 2019 · External reference
Turbine vane endwall film cooling comparison from five film-hole design patterns and three upstream injection angles
10.1115/1.4042057 · 2019 · External reference
Film-cooling effectiveness on a turbine blade platform with various hole shapes and layouts
2024 · External reference
Design of full-scale endwall film cooling of a turbine vane
10.1115/1.4045069 · 2020 · External reference
Comparisons of endwall overall effectiveness from two film hole distribution patterns at low and high exit mach numbers
10.1115/1.4047809 · 2020 · External reference
Using hydrogen as gas turbine fuel: premixed versus diffusive flame combustors
10.1115/1.4026085 · 2014 · External reference
Combined effects of the inlet temperature and species distortion on hydrogen turbines aero-thermal performance
10.1177/0957650915621416 · 2016 · External reference
A numerical investigation on the influence of trench holes upon the film cooling effectiveness of hydrogen and ammonia-enriched gas turbine vanes
2024 · External reference
Effects of water vapor concentration on the film cooling effectiveness of hydrogen gas turbine vane
2025 · External reference
Hydrogen combustion in two-stage high-pressure gas turbine—thermal and flow simulations for performance comparison with fossil fuels
10.1177/14680874231196987 · 2024 · External reference
Targeting full-hydrogen operation on industrial-scale gas turbines: impact of unconventional fuels on turbine module performance and aeromechanics
10.1115/1.4067127 · 2025 · External reference
10.1115/gt2016-56402
10.1115/gt2016-56402 · External reference
Bulk flow pulsations and film cooling—part I: injectant behavior
10.1016/0017-9310(95)00286-3 · 1996 · External reference
Bulk flow pulsations and film cooling—part II: flow structure and film effectiveness
10.1016/0017-9310(95)00287-1 · 1996 · External reference
Experimental study of periodic free stream unsteadiness effects on discrete hole film cooling in two geometries
10.1115/1.4041866 · 2019 · External reference
Experimental and numerical investigations on transient film cooling performances with trenched holes considering mainstream oscillation
2024 · External reference
10.1115/gt2018-75440
10.1115/gt2018-75440 · External reference
Characterizing hydrogen-fuelled pulsating combustion on thermodynamic properties of a combustor
10.1038/s42005-019-0142-8 · 2019 · External reference
On the observation of high-order, multi-mode, thermo-acoustic combustion instability in a model gas turbine combustor firing hydrogen containing syngases
10.1016/j.ijhydene.2019.02.113 · 2019 · External reference
Reduction of data from thin-film heat-transfer gauges: a concise numerical technique
10.2514/3.3486 · 1966 · External reference
A novel transient technique to determine recovery temperature, heat transfer coefficient, and film cooling effectiveness simultaneously in a transonic turbine cascade
10.1115/1.4029098 · 2015 · External reference
Unresolved reference
2012 · External reference
Describing the uncertainties in experimental results
10.1016/0894-1777(88)90043-x · 1988 · External reference
Unresolved reference
External reference
Experimental study of the endwall heat transfer of a transonic nozzle guide vane with upstream jet purge cooling part I—effect of density ratio
2022 · External reference
Experimental study of the endwall heat transfer of a transonic nozzle guide vane with upstream jet purge cooling part II—effect of combustor-NGV misalignment
2022 · External reference
Endwall heat transfer and cooling performance of a transonic turbine vane with upstream injection flow
10.1115/1.4052457 · 2022 · External reference
Bulk flow pulsations and film cooling—part I: injectant behavior
10.1016/0017-9310(95)00286-3 · ExternalCitation · doi-reference
Bulk flow pulsations and film cooling—part II: flow structure and film effectiveness
10.1016/0017-9310(95)00287-1 · ExternalCitation · doi-reference
Describing the uncertainties in experimental results
10.1016/0894-1777(88)90043-x · ExternalCitation · doi-reference
Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection
10.1016/j.ijheatmasstransfer.2018.12.079 · ExternalCitation · doi-reference
Influence of endwall 2D contouring on endwall adiabatic cooling effectiveness and aerodynamic performance
10.1016/j.ijheatmasstransfer.2019.02.089 · ExternalCitation · doi-reference
Research advances on mist assisted impingement and film cooling of turbine blades
10.1016/j.ijheatmasstransfer.2024.125907 · ExternalCitation · doi-reference
On the observation of high-order, multi-mode, thermo-acoustic combustion instability in a model gas turbine combustor firing hydrogen containing syngases
10.1016/j.ijhydene.2019.02.113 · ExternalCitation · doi-reference
Characterizing hydrogen-fuelled pulsating combustion on thermodynamic properties of a combustor
10.1038/s42005-019-0142-8 · ExternalCitation · doi-reference
Using hydrogen as gas turbine fuel
10.1115/1.1787513 · ExternalCitation · doi-reference
Flow visualization in a linear turbine cascade of high-performance turbine blades
10.1115/1.2841006 · ExternalCitation · doi-reference
Using hydrogen as gas turbine fuel: premixed versus diffusive flame combustors
10.1115/1.4026085 · ExternalCitation · doi-reference
A novel transient technique to determine recovery temperature, heat transfer coefficient, and film cooling effectiveness simultaneously in a transonic turbine cascade
10.1115/1.4029098 · ExternalCitation · doi-reference
Experimental study of periodic free stream unsteadiness effects on discrete hole film cooling in two geometries
10.1115/1.4041866 · ExternalCitation · doi-reference
Turbine vane endwall film cooling comparison from five film-hole design patterns and three upstream injection angles
10.1115/1.4042057 · ExternalCitation · doi-reference
Design of full-scale endwall film cooling of a turbine vane
10.1115/1.4045069 · ExternalCitation · doi-reference
Comparisons of endwall overall effectiveness from two film hole distribution patterns at low and high exit mach numbers
10.1115/1.4047809 · ExternalCitation · doi-reference
Endwall heat transfer and cooling performance of a transonic turbine vane with upstream injection flow
10.1115/1.4052457 · ExternalCitation · doi-reference
The effects of axisymmetric convergent contouring and blowing ratio on endwall film cooling and vane pressure side surface phantom cooling performance
10.1115/1.4052500 · ExternalCitation · doi-reference
Targeting full-hydrogen operation on industrial-scale gas turbines: impact of unconventional fuels on turbine module performance and aeromechanics
10.1115/1.4067127 · ExternalCitation · doi-reference
Review of the impact of hydrogen-containing fuels on gas turbine hot-section materials
10.1115/1.4067335 · ExternalCitation · doi-reference
10.1115/2000-gt-0201
10.1115/2000-gt-0201 · ExternalCitation · doi-reference
10.1115/gt2016-56402
10.1115/gt2016-56402 · ExternalCitation · doi-reference
10.1115/gt2018-75440
10.1115/gt2018-75440 · ExternalCitation · doi-reference
10.1115/imece2017-72157
10.1115/imece2017-72157 · ExternalCitation · doi-reference
Combined effects of the inlet temperature and species distortion on hydrogen turbines aero-thermal performance
10.1177/0957650915621416 · ExternalCitation · doi-reference
Hydrogen combustion in two-stage high-pressure gas turbine—thermal and flow simulations for performance comparison with fossil fuels
10.1177/14680874231196987 · ExternalCitation · doi-reference
Reduction of data from thin-film heat-transfer gauges: a concise numerical technique
10.2514/3.3486 · ExternalCitation · doi-reference
