Effects of area ratio and mean rise angle on the aerodynamics of inter-turbine ducts

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1115/GT2014-27207
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Name affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
  2. National Research Council of Canada. Aerospace
FormatText, Article
Proceedings titleProceedings of the ASME Turbo Expo
ConferenceASME Turbo Expo 2014: Turbine Technical Conference and Exposition, GT 2014, 16 June 2014 through 20 June 2014
SubjectAerodynamics; Boundary layer flow; Pressure gradient; Reynolds number; Turbines; Vortex flow; Adverse pressure gradient; Boundary-layer separation; Computational studies; Counter-rotating vortices; Pressure loss; Static pressure; Upstream wake; Ducts
Publication date
PublisherAmerican Society of Mechanical Engineers
Peer reviewedYes
NPARC number21275616
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Record identifier7665e5dd-44e8-41bd-b8bb-1f64dc3b0d69
Record created2015-07-14
Record modified2020-04-22
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