Experiments of transpiration cooling inspired panel cooling on a turbine blade yielding film effectiveness levels over 95%
Panels were tested at different locations around the turbine blade, on both suction and pressure surfaces. Three different surface porosities were also tested. Results demonstrated that the approach can be very successful with high levels of film cooling effectiveness, exceeding 95%, achieved using...
Main Authors: | , , , |
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Format: | Journal article |
Language: | English |
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MDPI
2021
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_version_ | 1797107268785799168 |
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author | Wambersie, A Wong, H Ireland, P Mayo, I |
author_facet | Wambersie, A Wong, H Ireland, P Mayo, I |
author_sort | Wambersie, A |
collection | OXFORD |
description | Panels were tested at different locations around the turbine blade, on both suction and pressure surfaces. Three different surface porosities were also tested. Results demonstrated that the approach can be very successful with high levels of film cooling effectiveness, exceeding 95%, achieved using low coolant mass flow rates. Increasing the surface porosity also proved to be an important parameter in the panel’s performance. Additionally, staggering the film holes lead to significant positive interactions between individual films, resulting in much improved panel performance. |
first_indexed | 2024-03-07T07:13:40Z |
format | Journal article |
id | oxford-uuid:4a84aefb-dfa5-4994-ae6e-fa3ebd544af4 |
institution | University of Oxford |
language | English |
last_indexed | 2024-03-07T07:13:40Z |
publishDate | 2021 |
publisher | MDPI |
record_format | dspace |
spelling | oxford-uuid:4a84aefb-dfa5-4994-ae6e-fa3ebd544af42022-07-21T15:40:03ZExperiments of transpiration cooling inspired panel cooling on a turbine blade yielding film effectiveness levels over 95%Journal articlehttp://purl.org/coar/resource_type/c_dcae04bcuuid:4a84aefb-dfa5-4994-ae6e-fa3ebd544af4EnglishSymplectic ElementsMDPI2021Wambersie, AWong, HIreland, PMayo, IPanels were tested at different locations around the turbine blade, on both suction and pressure surfaces. Three different surface porosities were also tested. Results demonstrated that the approach can be very successful with high levels of film cooling effectiveness, exceeding 95%, achieved using low coolant mass flow rates. Increasing the surface porosity also proved to be an important parameter in the panel’s performance. Additionally, staggering the film holes lead to significant positive interactions between individual films, resulting in much improved panel performance. |
spellingShingle | Wambersie, A Wong, H Ireland, P Mayo, I Experiments of transpiration cooling inspired panel cooling on a turbine blade yielding film effectiveness levels over 95% |
title | Experiments of transpiration cooling inspired panel cooling on a turbine blade yielding film effectiveness levels over 95% |
title_full | Experiments of transpiration cooling inspired panel cooling on a turbine blade yielding film effectiveness levels over 95% |
title_fullStr | Experiments of transpiration cooling inspired panel cooling on a turbine blade yielding film effectiveness levels over 95% |
title_full_unstemmed | Experiments of transpiration cooling inspired panel cooling on a turbine blade yielding film effectiveness levels over 95% |
title_short | Experiments of transpiration cooling inspired panel cooling on a turbine blade yielding film effectiveness levels over 95% |
title_sort | experiments of transpiration cooling inspired panel cooling on a turbine blade yielding film effectiveness levels over 95 |
work_keys_str_mv | AT wambersiea experimentsoftranspirationcoolinginspiredpanelcoolingonaturbinebladeyieldingfilmeffectivenesslevelsover95 AT wongh experimentsoftranspirationcoolinginspiredpanelcoolingonaturbinebladeyieldingfilmeffectivenesslevelsover95 AT irelandp experimentsoftranspirationcoolinginspiredpanelcoolingonaturbinebladeyieldingfilmeffectivenesslevelsover95 AT mayoi experimentsoftranspirationcoolinginspiredpanelcoolingonaturbinebladeyieldingfilmeffectivenesslevelsover95 |