Flow control in an aggressive inter-turbine duct using low profile vortex generators

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1115/GT2012-69951
AuthorSearch for: 1; Search for: 1; Search for: 1; Search for: 1; Search for: 1
Affiliation
  1. National Research Council of Canada. Aerospace
FormatText, Article
ConferenceASME Turbo Expo 2012: Turbine Technical Conference and Exposition, GT 2012, June 11-15, 2012, Copenhagen, Denmark
SubjectBoundary-layer separation; Casing boundary layer; Counter-rotating vortices; Experimental investigations; Flow mechanisms; Streamwise vortices; Total-pressure loss; Vortex generators; Boundary layers; Ducts; Three dimensional; Transport aircraft; Vortex flow; Gas turbines
Abstract
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LanguageEnglish
Peer reviewedYes
NPARC number21270197
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Record identifier3307890f-9e98-4a8d-975e-159d3748d3d2
Record created2014-01-10
Record modified2020-04-21
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