Endwall flow patterns and film cooling performance under pulsatile conditions of hydrogen-combustion turbines

Endwall heat transfer and cooling performance of a transonic turbine vane with upstream injection flow

10.1115/1.4052457 · doi-reference

Describing the uncertainties in experimental results

10.1016/0894-1777(88)90043-x · 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 · doi-reference

Reduction of data from thin-film heat-transfer gauges: a concise numerical technique

10.2514/3.3486 · 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 · doi-reference

Characterizing hydrogen-fuelled pulsating combustion on thermodynamic properties of a combustor

10.1038/s42005-019-0142-8 · doi-reference

10.1115/gt2018-75440

10.1115/gt2018-75440 · doi-reference

Experimental study of periodic free stream unsteadiness effects on discrete hole film cooling in two geometries

10.1115/1.4041866 · doi-reference

Bulk flow pulsations and film cooling—part II: flow structure and film effectiveness

10.1016/0017-9310(95)00287-1 · doi-reference

Bulk flow pulsations and film cooling—part I: injectant behavior

10.1016/0017-9310(95)00286-3 · doi-reference

10.1115/gt2016-56402

10.1115/gt2016-56402 · 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 · doi-reference

Hydrogen combustion in two-stage high-pressure gas turbine—thermal and flow simulations for performance comparison with fossil fuels

10.1177/14680874231196987 · doi-reference

Combined effects of the inlet temperature and species distortion on hydrogen turbines aero-thermal performance

10.1177/0957650915621416 · doi-reference

Using hydrogen as gas turbine fuel: premixed versus diffusive flame combustors

10.1115/1.4026085 · doi-reference

Comparisons of endwall overall effectiveness from two film hole distribution patterns at low and high exit mach numbers

10.1115/1.4047809 · doi-reference

Design of full-scale endwall film cooling of a turbine vane

10.1115/1.4045069 · doi-reference

Turbine vane endwall film cooling comparison from five film-hole design patterns and three upstream injection angles

10.1115/1.4042057 · doi-reference

Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection

10.1016/j.ijheatmasstransfer.2018.12.079 · doi-reference

10.1115/imece2017-72157

10.1115/imece2017-72157 · doi-reference

Research advances on mist assisted impingement and film cooling of turbine blades

10.1016/j.ijheatmasstransfer.2024.125907 · 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 · doi-reference

Influence of endwall 2D contouring on endwall adiabatic cooling effectiveness and aerodynamic performance

10.1016/j.ijheatmasstransfer.2019.02.089 · doi-reference

10.1115/2000-gt-0201

10.1115/2000-gt-0201 · doi-reference

Flow visualization in a linear turbine cascade of high-performance turbine blades

10.1115/1.2841006 · doi-reference

Using hydrogen as gas turbine fuel

10.1115/1.1787513 · doi-reference

Review of the impact of hydrogen-containing fuels on gas turbine hot-section materials

10.1115/1.4067335 · doi-reference