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

doi:10.1115/GT2002-30662

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

Mechanical Engineering

Research output: Contribution to conference › Paper › peer-review

13 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 language	English (US)
Pages	1191-1199
Number of pages	9
DOIs	https://doi.org/10.1115/GT2002-30662
State	Published - 2002
Event	Proceedings of the ASME TURBO EXPO 2002: Turbomachinery - Amsterdam, Netherlands Duration: Jun 3 2002 → Jun 6 2002

Other

Other	Proceedings of the ASME TURBO EXPO 2002: Turbomachinery
Country/Territory	Netherlands
City	Amsterdam
Period	6/3/02 → 6/6/02

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title = "Using Gurney flaps to control laminar separation on linear cascade blades",

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.",

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T1 - Using Gurney flaps to control laminar separation on linear cascade blades

AU - Byerley, Aaron R.

AU - Störmer, Oliver

AU - Baughn, James W.

AU - Simon, Terrence W.

AU - Van Treuren, Kenneth W.

AU - List, Jörg

PY - 2002

Y1 - 2002

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AB - 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.

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T2 - Proceedings of the ASME TURBO EXPO 2002: Turbomachinery

Y2 - 3 June 2002 through 6 June 2002

ER -

Using Gurney flaps to control laminar separation on linear cascade blades

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