Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade

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This thesis investigates and improves a film cooling configuration for a high-pressure turbine blade operating under transonic conditions. Using computational fluid dynamics validated with experimental data, several geometric parameters are analyzed through sensitivity studies. The results identify...

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Autor principal: Giménez, Juan Ignacio
Formato: Tesis de maestría
Lenguaje:en_US
Publicado: Instituto Tecnológico de Buenos Aires (ITBA) 2026
Materias:
FILM COOLING, HIGH-PRESSURE TURBINE BLADE, GAS TURBINE COOLING, HEAT TRANSFER
ENFRIAMIENTO POR PELÍCULA, ÁLABE DE TURBINA DE ALTA PRESIÓN, ENFRIAMIENTO DE TURBINAS DE GAS, TRANSFERENCIA DE CALOR, EFECTIVIDAD DEL ENFRIAMIENTO POR PELÍCULA
Acceso en línea:https://hdl.handle.net/20.500.14769/5269
Aporte de:
Repositorio Institucional Instituto Tecnológico de Buenos Aires (ITBA) de Instituto Tecnológico de Buenos Aires (ITBA)
id I32-R138-20.500.14769-5269
record_format dspace
spelling I32-R138-20.500.14769-52692026-03-17T07:32:46Z Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade Giménez, Juan Ignacio FILM COOLING, HIGH-PRESSURE TURBINE BLADE, GAS TURBINE COOLING, HEAT TRANSFER ENFRIAMIENTO POR PELÍCULA, ÁLABE DE TURBINA DE ALTA PRESIÓN, ENFRIAMIENTO DE TURBINAS DE GAS, TRANSFERENCIA DE CALOR, EFECTIVIDAD DEL ENFRIAMIENTO POR PELÍCULA This thesis investigates and improves a film cooling configuration for a high-pressure turbine blade operating under transonic conditions. Using computational fluid dynamics validated with experimental data, several geometric parameters are analyzed through sensitivity studies. The results identify optimized cooling configurations that reduce blade temperatures and improve film cooling effectiveness with minimal aerodynamic penalties. 2026-03-16T17:26:21Z 2026-03-16T17:26:21Z 2026-09 Tesis de maestría https://hdl.handle.net/20.500.14769/5269 en_US application/pdf Instituto Tecnológico de Buenos Aires (ITBA)
institution Instituto Tecnológico de Buenos Aires (ITBA)
institution_str I-32
repository_str R-138
collection Repositorio Institucional Instituto Tecnológico de Buenos Aires (ITBA)
language en_US
topic FILM COOLING, HIGH-PRESSURE TURBINE BLADE, GAS TURBINE COOLING, HEAT TRANSFER
ENFRIAMIENTO POR PELÍCULA, ÁLABE DE TURBINA DE ALTA PRESIÓN, ENFRIAMIENTO DE TURBINAS DE GAS, TRANSFERENCIA DE CALOR, EFECTIVIDAD DEL ENFRIAMIENTO POR PELÍCULA
spellingShingle FILM COOLING, HIGH-PRESSURE TURBINE BLADE, GAS TURBINE COOLING, HEAT TRANSFER
ENFRIAMIENTO POR PELÍCULA, ÁLABE DE TURBINA DE ALTA PRESIÓN, ENFRIAMIENTO DE TURBINAS DE GAS, TRANSFERENCIA DE CALOR, EFECTIVIDAD DEL ENFRIAMIENTO POR PELÍCULA
Giménez, Juan Ignacio
Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade
topic_facet FILM COOLING, HIGH-PRESSURE TURBINE BLADE, GAS TURBINE COOLING, HEAT TRANSFER
ENFRIAMIENTO POR PELÍCULA, ÁLABE DE TURBINA DE ALTA PRESIÓN, ENFRIAMIENTO DE TURBINAS DE GAS, TRANSFERENCIA DE CALOR, EFECTIVIDAD DEL ENFRIAMIENTO POR PELÍCULA
description This thesis investigates and improves a film cooling configuration for a high-pressure turbine blade operating under transonic conditions. Using computational fluid dynamics validated with experimental data, several geometric parameters are analyzed through sensitivity studies. The results identify optimized cooling configurations that reduce blade temperatures and improve film cooling effectiveness with minimal aerodynamic penalties.
format Tesis de maestría
author Giménez, Juan Ignacio
author_facet Giménez, Juan Ignacio
author_sort Giménez, Juan Ignacio
title Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade
title_short Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade
title_full Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade
title_fullStr Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade
title_full_unstemmed Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade
title_sort sensitivity study and improvement of a film cooling configuration of a high-pressure turbine blade
publisher Instituto Tecnológico de Buenos Aires (ITBA)
publishDate 2026
url https://hdl.handle.net/20.500.14769/5269
work_keys_str_mv AT gimenezjuanignacio sensitivitystudyandimprovementofafilmcoolingconfigurationofahighpressureturbineblade
_version_ 1865139177069215744

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