Reynolds analog in combustor modeling

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1115/GT2007-27017
AuthorSearch for: 1ORCID identifier: https://orcid.org/0009-0008-0777-7919; Search for: 1
Affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
FormatText, Article
ConferenceASME Turbo Expo 2007 - Power for Land, Sea and Air, May 14-17, 2007, Montreal, Quebec, Canada
SubjectReynolds anlogy; turbulent scalar transfer; combustor modeling; schmidt number; prandti number
Abstract
Publication date
PublisherAmerican Society of Mechanical Engineers (ASME)
In
Peer reviewedYes
NRC numberGTL-2007-0006
NPARC number8933892
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Record identifier57052910-3ba8-47af-bcc4-aa1ffb1b7d77
Record created2009-04-23
Record modified2025-11-18
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