The Influence of Reynolds Number, Turbulence Intensity and Length Scale on Separated-Flow Transition of a Low-Pressure Turbine Airfoil

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ConferenceASME TurboExpo 2004 from June 14, 2004 to June 17, 2004, Vienna, Austria
SubjectHigh-lift low-pressure turbine blade; Transition; Low Reynolds number; Laminar separation
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
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Peer reviewedYes
NRC numberAL-2003-0076
NPARC number8932709
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Record identifiera7eadb11-2d8a-47ef-86ec-4a8521484aed
Record created2009-04-23
Record modified2016-05-09
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