Influences of inlet swirl distributions on an inter-turbine duct part I: Casing swirl variation

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1115/GT2011-45554
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Affiliation
  1. National Research Council of Canada
FormatText, Article
ConferenceASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011, 6 June 2011 through 10 June 2011, Vancouver, BC
SubjectAdverse pressure gradient; Aerodynamic performance; Blade tip vortex; Boundary-layer separation; Casing boundary layer; Counter-rotating vortices; Engine weight; Experimental data; Flow behaviors; Flow development; Flow physics; Inlet swirls; Swirl angles; Total pressure coefficients; Transition ducts; Turbine blade; Turbulence intensity; Wake flows; Boundary layers; Ducts; Exhibitions; Pressure gradient; Three dimensional; Turbomachine blades; Vortex flow; Wakes; Aerodynamics
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LanguageEnglish
Peer reviewedYes
NPARC number21271724
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