Isolating influences of varying pitch from the effects of non-zero compound angles on effusion cooling

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DOIResolve DOI: https://doi.org/10.1017/aer.2024.108
AuthorSearch for: 1ORCID identifier: https://orcid.org/0009-0001-7614-8947; Search for: 1; Search for: ORCID identifier: https://orcid.org/0009-0007-4294-2142; Search for: ORCID identifier: https://orcid.org/0000-0003-3194-3549; Search for: 1ORCID identifier: https://orcid.org/0000-0003-4601-0370; Search for: 1ORCID identifier: https://orcid.org/0000-0001-8028-0214; Search for: 1ORCID identifier: https://orcid.org/0000-0002-6622-5830
Affiliation
  1. National Research Council Canada. Aerospace
FormatText, Article
Subjectgas turbine; film cooling; effusion cooling; AFE (adiabatic film cooling effectiveness); PSP (pressure sensitive paint); compound angle; pitch
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PublisherCambridge University Press
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LanguageEnglish
Peer reviewedYes
IdentifierS0001924024001088
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Record identifier302e48d9-9998-47a7-b5ad-13e1c56a285e
Record created2025-09-09
Record modified2025-09-10
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