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Boundary layer transition and convective heat transfer of the high-pressure turbine vane LS89

immc | Louvain-la-Neuve

immc
20 April 2021, modified on 18 December 2024

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Boundary layer transition and convective heat transfer of the high-pressure turbine vane LS89
29 Apr
Boundary layer transition and convective heat transfer of the high-pressure turbine vane LS89 by Tânia Sofia CAÇÃO FERREIRA Pour l’obtention du grade de Docteur en sciences de l’ingénieur et technologie Boundary layer transition from laminar to turbulent generates high levels of shear stresses and heat transfer rates, influencing the overall efficiency of the aircraft engine.
Placeholder image
Boundary layer transition and convective heat transfer of the high-pressure turbine vane LS89
29 Apr
Boundary layer transition and convective heat transfer of the high-pressure turbine vane LS89 by Tânia Sofia CAÇÃO FERREIRA Pour l’obtention du grade de Docteur en sciences de l’ingénieur et technologie Boundary layer transition from laminar to turbulent generates high levels of shear stresses and heat transfer rates, influencing the overall efficiency of the aircraft engine.