Prandtl/Schmidt number effect on temperature distribution in a generic combustor

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1016/j.ijthermalsci.2008.03.014
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
Subjectturbulence scalar transfer; combustor modeling; Schmidt number; Prandtl number; Reynolds analogy
Abstract
Publication date
PublisherElsevier
In
LanguageEnglish
Peer reviewedYes
IdentifierS1290072908000720
Export citationExport as RIS
Report a correctionReport a correction (opens in a new tab)
Record identifier21c0d528-8ae0-4b38-9d5a-1a38c7e79b49
Record created2024-12-18
Record modified2024-12-18
Date modified: