Flow control in an aggressive interturbine transition duct using low profile vortex generators

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1115/1.4027656
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Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
  2. National Research Council of Canada. Aerospace
FormatText, Article
SubjectBoundary layers; Flow control; Reynolds number; Transport aircraft; Adverse pressure gradient; Boundary-layer separation; Casing boundary layer; Co-rotating vortices; Counter-rotating vortices; Experimental investigations; Overall pressure loss; Turbulence intensity; Ducts
Abstract
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LanguageEnglish
Peer reviewedYes
NPARC number21272811
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Record identifierbe0cbbac-62bf-4c20-8dc1-daee51409019
Record created2014-12-03
Record modified2020-04-22
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