Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface

The paper presents numerical heat-transfer correlations established from numerical CFD study of a 3D hotair jet array impinging on curved (circular) surface. The results are in the form of numerical correlations for the average and maximum Nusselt number for different nozzle-to-nozzle spacing, nozzl...

وصف كامل

محفوظ في:
التفاصيل البيبلوغرافية
المؤلف الرئيسي: Fregeau, M (author)
مؤلفون آخرون: Saeed, F (author), Paraschivoiu, I. (author), unknown (author)
التنسيق: article
منشور في: 2005
الموضوعات:
الوصول للمادة أونلاين:https://eprints.kfupm.edu.sa/id/eprint/815/1/AIAAJ-MathieuFregeau1stRevision.pdf
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_version_ 1864513389207748608
author Fregeau, M
author2 Saeed, F
Paraschivoiu, I.
unknown
author2_role author
author
author
author_facet Fregeau, M
Saeed, F
Paraschivoiu, I.
unknown
author_role author
dc.creator.none.fl_str_mv Fregeau, M
Saeed, F
Paraschivoiu, I.
unknown
dc.date.none.fl_str_mv 2005-05-01
2020
dc.format.none.fl_str_mv application/pdf
dc.identifier.none.fl_str_mv https://eprints.kfupm.edu.sa/id/eprint/815/1/AIAAJ-MathieuFregeau1stRevision.pdf
(2005) Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface. AIAA Journal of Aircraft, 42 (3). pp. 665-670.
dc.language.none.fl_str_mv en
dc.publisher.none.fl_str_mv AIAA
dc.relation.none.fl_str_mv https://eprints.kfupm.edu.sa/id/eprint/815/
dc.rights.*.fl_str_mv info:eu-repo/semantics/openAccess
dc.subject.none.fl_str_mv Aerospace
Mechanical
dc.title.none.fl_str_mv Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface
dc.type.none.fl_str_mv Article
PeerReviewed
info:eu-repo/semantics/publishedVersion
info:eu-repo/semantics/article
description The paper presents numerical heat-transfer correlations established from numerical CFD study of a 3D hotair jet array impinging on curved (circular) surface. The results are in the form of numerical correlations for the average and maximum Nusselt number for different nozzle-to-nozzle spacing, nozzle-to-surface height and hot-air jet mach numbers typical of those in an hot-air anti-icing system employed on aircraft wings. The paper presents a validation case and show that the results obtained from the CFD study are in good agreement with experimental data found in literature. The paper presents an interpolation technique, the dual Kriging method, that make use of the numerical database for anti-icing simulation on aircraft wings. The benefit of using the dual Kriging method is that it preserves the non-linear nature of the heat-transfer distribution from a hot-air jet impinging on a curved surface.
eu_rights_str_mv openAccess
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id KFUPM_12dcbe511f68ca79a43f8a4d18999c0b
identifier_str_mv (2005) Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface. AIAA Journal of Aircraft, 42 (3). pp. 665-670.
language_invalid_str_mv en
network_acronym_str KFUPM
network_name_str King Fahd University of Petroleum and Minerals
oai_identifier_str oai::815
publishDate 2005
publisher.none.fl_str_mv AIAA
repository.mail.fl_str_mv
repository.name.fl_str_mv
repository_id_str
spelling Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave SurfaceFregeau, MSaeed, FParaschivoiu, I.unknownAerospaceMechanicalThe paper presents numerical heat-transfer correlations established from numerical CFD study of a 3D hotair jet array impinging on curved (circular) surface. The results are in the form of numerical correlations for the average and maximum Nusselt number for different nozzle-to-nozzle spacing, nozzle-to-surface height and hot-air jet mach numbers typical of those in an hot-air anti-icing system employed on aircraft wings. The paper presents a validation case and show that the results obtained from the CFD study are in good agreement with experimental data found in literature. The paper presents an interpolation technique, the dual Kriging method, that make use of the numerical database for anti-icing simulation on aircraft wings. The benefit of using the dual Kriging method is that it preserves the non-linear nature of the heat-transfer distribution from a hot-air jet impinging on a curved surface.AIAA2005-05-012020ArticlePeerReviewedinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttps://eprints.kfupm.edu.sa/id/eprint/815/1/AIAAJ-MathieuFregeau1stRevision.pdf (2005) Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface. AIAA Journal of Aircraft, 42 (3). pp. 665-670. enhttps://eprints.kfupm.edu.sa/id/eprint/815/info:eu-repo/semantics/openAccessoai::8152019-11-01T13:25:23Z
spellingShingle Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface
Fregeau, M
Aerospace
Mechanical
status_str publishedVersion
title Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface
title_full Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface
title_fullStr Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface
title_full_unstemmed Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface
title_short Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface
title_sort Numerical Correlations for Heat Transfer From an Array of Hot-Air Jets Impinging on a 3D Concave Surface
topic Aerospace
Mechanical
url https://eprints.kfupm.edu.sa/id/eprint/815/1/AIAAJ-MathieuFregeau1stRevision.pdf