Influence of Vortex Generator Jet-Induced Transition on Separating Low Pressure Turbine Boundary Layers

Author:

Reimann Daniel1,Bloxham Matthew1,Crapo Katie1,Pluim Jonathan1,Bons Jeffrey1

Affiliation:

1. Brigham Young University

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

1. [1]Matsunuma,T.,Abe,H.,Tsutsui,Y.,andMurata,K.,1998,"CharacteristicsofanAnnularTurbine CascadeatLowReynoldsNumbers.",presented atIGTI1998 in Stockholm, Sweden,June1998,paper #98-GT-518.

2. [2]DanHelton, 1997,privatecommunication.

3. [3]Sharma, O., 1998, "Impact ofReynoldsNumberon LPTurbine Performance,"Proc.Of1997 MinnowbrookIIWorkshoponBoundaryLayerTransitioninTurbomachines,NASA/CP-1998-206958.

4. [4]Sondergaard,R.,Bons,J.P.,andRivir,R. B.,2002,"ControlofLow-PressureTurbineSeparation UsingVortexGeneratorJets,"AIAAJ.PropulsionandPower, Vol.18,No.4, Jul/Aug2002. pp.889-895.

5. [5]Praisner,T.J.andClark,J.P.,2004,"PredictingTransitioninTurbomachinery,Part1-AReviewand NewModelDevelopment,"ASMEPaperNo.GT-2004-54108.

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