Using Gurney flaps to control laminar separation on linear cascade blades

Aaron R. Byerley, Oliver Störmer, James W. Baughn, Terrence W. Simon, Kenneth W. Van Treuren, Jörg List

Research output: Contribution to conferencePaperpeer-review

12 Scopus citations

Abstract

The effect of Gurney flaps for three Reynolds number conditions was determined. Separation was expected at two lower reynolds numbers of 28x103 and 65x103. Fully attached flow was expected at 167x103. The freestream turbulence was held constant at 0.8% during these experiments. The resultant data were analyzed in detail.

Original languageEnglish (US)
Pages1191-1199
Number of pages9
DOIs
StatePublished - Dec 1 2002
EventProceedings of the ASME TURBO EXPO 2002: Turbomachinery - Amsterdam, Netherlands
Duration: Jun 3 2002Jun 6 2002

Other

OtherProceedings of the ASME TURBO EXPO 2002: Turbomachinery
Country/TerritoryNetherlands
CityAmsterdam
Period6/3/026/6/02

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