Heat flux augmentation caused by surface imperfections in turbulent boundary layers

Aerodynamic heating of hypersonic vehicles is one of the key challenges needed to be overcome in the pursuit of hypersonic ascent, re-entry, or sustained flight. Small, unavoidable imperfections are always present on the surface of aircraft in the form of steps, gaps, and protuberances. These can le...

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Main Authors: Ivison, W, Hambidge, CJ, McGilvray, M, Flinton, A, Merrifield, J, Steelant, J
Format: Conference item
Language:English
Published: Council of European Aerospace Societies 2024
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author Ivison, W
Hambidge, CJ
McGilvray, M
Flinton, A
Merrifield, J
Steelant, J
author_facet Ivison, W
Hambidge, CJ
McGilvray, M
Flinton, A
Merrifield, J
Steelant, J
author_sort Ivison, W
collection OXFORD
description Aerodynamic heating of hypersonic vehicles is one of the key challenges needed to be overcome in the pursuit of hypersonic ascent, re-entry, or sustained flight. Small, unavoidable imperfections are always present on the surface of aircraft in the form of steps, gaps, and protuberances. These can lead to high levels of localised heat flux augmentation, up to many times the undisturbed level. Flat plate experiments have been carried out in the Oxford High Density Tunnel with the aim of characterising the heating effects caused by small scale protuberances and steps in turbulent boundary layers. The current work presents experimental heat flux augmentation data, an assessment of existing heat flux correlations, and introduces new engineering level correlations to describe heat flux augmentation for a range of surface geometries.
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spelling oxford-uuid:51170456-e7a1-4cc3-8080-3fdbcda475322024-07-17T13:55:28ZHeat flux augmentation caused by surface imperfections in turbulent boundary layersConference itemhttp://purl.org/coar/resource_type/c_5794uuid:51170456-e7a1-4cc3-8080-3fdbcda47532EnglishSymplectic ElementsCouncil of European Aerospace Societies2024Ivison, WHambidge, CJMcGilvray, MFlinton, AMerrifield, JSteelant, JAerodynamic heating of hypersonic vehicles is one of the key challenges needed to be overcome in the pursuit of hypersonic ascent, re-entry, or sustained flight. Small, unavoidable imperfections are always present on the surface of aircraft in the form of steps, gaps, and protuberances. These can lead to high levels of localised heat flux augmentation, up to many times the undisturbed level. Flat plate experiments have been carried out in the Oxford High Density Tunnel with the aim of characterising the heating effects caused by small scale protuberances and steps in turbulent boundary layers. The current work presents experimental heat flux augmentation data, an assessment of existing heat flux correlations, and introduces new engineering level correlations to describe heat flux augmentation for a range of surface geometries.
spellingShingle Ivison, W
Hambidge, CJ
McGilvray, M
Flinton, A
Merrifield, J
Steelant, J
Heat flux augmentation caused by surface imperfections in turbulent boundary layers
title Heat flux augmentation caused by surface imperfections in turbulent boundary layers
title_full Heat flux augmentation caused by surface imperfections in turbulent boundary layers
title_fullStr Heat flux augmentation caused by surface imperfections in turbulent boundary layers
title_full_unstemmed Heat flux augmentation caused by surface imperfections in turbulent boundary layers
title_short Heat flux augmentation caused by surface imperfections in turbulent boundary layers
title_sort heat flux augmentation caused by surface imperfections in turbulent boundary layers
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AT hambidgecj heatfluxaugmentationcausedbysurfaceimperfectionsinturbulentboundarylayers
AT mcgilvraym heatfluxaugmentationcausedbysurfaceimperfectionsinturbulentboundarylayers
AT flintona heatfluxaugmentationcausedbysurfaceimperfectionsinturbulentboundarylayers
AT merrifieldj heatfluxaugmentationcausedbysurfaceimperfectionsinturbulentboundarylayers
AT steelantj heatfluxaugmentationcausedbysurfaceimperfectionsinturbulentboundarylayers