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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  1. National Research Council of Canada. NRC Institute for Aerospace Research
  2. National Research Council of Canada. Aerospace
FormatText, Article
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
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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