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Effect of Reynolds Number and Periodic Unsteady Wake Flow Condition on Boundary Layer Development, Separation, and Re-attachment along the Suction Surface of a Low Pressure Turbine BladeThe paper experimentally studies the effects of periodic unsteady wake flow and different Reynolds numbers on boundary layer development, separation and re-attachment along the suction surface of a low pressure turbine blade. The experimental investigations were performed on a large scale, subsonic unsteady turbine cascade research facility at Turbomachinery Performance and Flow Research Laboratory (TPFL) of Texas A&M University. The experiments were carried out at Reynolds numbers of 110,000 and 150,000 (based on suction surface length and exit velocity). One steady and two different unsteady inlet flow conditions with the corresponding passing frequencies, wake velocities, and turbulence intensities were investigated. The reduced frequencies chosen cover the operating range of LP turbines. In addition to the unsteady boundary layer measurements, surface pressure measurements were performed. The inception, onset, and the extent of the separation bubble information collected from the pressure measurements were compared with the hot wire measurements. The results presented in ensemble-averaged, and the contour plot forms help to understand the physics of the separation phenomenon under periodic unsteady wake flow and different Reynolds number. It was found that the suction surface displayed a strong separation bubble for these three different reduced frequencies. For each condition, the locations defining the separation bubble were determined carefully analyzing and examining the pressure and mean velocity profile data. The location of the boundary layer separation was dependent of the Reynolds number. It is observed that starting point of the separation bubble and the re-attachment point move further downstream by increasing Reynolds number from 110,000 to 150,000. Also, the size of the separation bubble is smaller when compared to that for Re=110,000.
Document ID
20100015672
Acquisition Source
Glenn Research Center
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Ozturk, B.
(Texas A&M Univ. College Station, TX, United States)
Schobeiri, M. T.
(Texas A&M Univ. College Station, TX, United States)
Ashpis, David E.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
June 6, 2005
Subject Category
Aerodynamics
Report/Patent Number
GT2005-68600
E-17178-P
Report Number: GT2005-68600
Report Number: E-17178-P
Meeting Information
Meeting: ASME Turbo Expo 2005: Power for Land, Sea and Air
Location: Reno, NV
Country: United States
Start Date: June 6, 2005
End Date: June 9, 2005
Sponsors: American Society of Mechanical Engineers
Funding Number(s)
CONTRACT_GRANT: NCC3-793
WBS: WBS 561581.02.08.03.21.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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