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Tesis

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

Giménez, Juan Ignacio · Instituto Tecnológico de Buenos Aires (ITBA) · 2026

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Author / responsible party
Giménez, Juan Ignacio
Publisher
Instituto Tecnológico de Buenos Aires (ITBA)
Year
2026
Language
en_US

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Summary

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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 optimized cooling configurations that reduce blade temperatures and improve film cooling effectiveness with minimal aerodynamic penalties.

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APA 7

Giménez, J. I. (2026). Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade. Instituto Tecnológico de Buenos Aires (ITBA). https://hdl.handle.net/20.500.14769/5269

MLA

Giménez, Juan Ignacio. Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade. Instituto Tecnológico de Buenos Aires (ITBA), 2026. https://hdl.handle.net/20.500.14769/5269.

Chicago

Giménez, Juan Ignacio. 2026. Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade. Instituto Tecnológico de Buenos Aires (ITBA). https://hdl.handle.net/20.500.14769/5269.

Harvard

Giménez, J. I. 2026, Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade, Instituto Tecnológico de Buenos Aires (ITBA), available at: https://hdl.handle.net/20.500.14769/5269 [Accessed 8 Aug. 2026].

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Resource details

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Title
Sensitivity Study and Improvement of a Film Cooling Configuration of a High-Pressure Turbine Blade
Author / contributors
Giménez, Juan Ignacio
Publisher
Instituto Tecnológico de Buenos Aires (ITBA)
Publication year
2026
Language
en_US

Subjects

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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
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