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Effects of Elevated Free-Stream Turbulence on Active Control of a Separation BubbleThe Effects of elevated free-stream turbulence (FST) on the natural and periodically excited separation bubbles were studied experimentally, due to the relevance of this flow to low-pressure turbine blades at low Reynolds numbers. A bubble was formed at the leading edge of a flat plate and the FST level was altered by placing a grid across the flow at different locations upstream of the plate. The mixing across the separated shear-layer, forming the free boundary of the bubble, increased due to the elevated FST and due to nominally two-dimensional periodic excitation, both flattening and shortening the bubble. Periodic excitation at frequencies that were at least an order of magnitude lower than those associated with the initial shear-layer instability, were very effective at low FST, because the amplitudes of the excitation frequency and its harmonic were amplified over the bubble. High frequency excitation (F+ 3, based on the length of the baseline low FST bubble) had a major effect close to the separation location, while farther downstream the excited fluctuations rapidly decayed in the reattachment region. Low frequency excitation, that generated waves comparable to the length of the unperturbed bubble (F+ 1) were less effective and their magnitude decayed at a slower rate downstream of reattachment. An increase in the level of the FST reduced the net effect of the periodic excitation on the mixing enhancement and subsequent reattachment process, probably due to a destructive interference between the nominally 2D excitation and the random (in space and time) FST, reducing the spanwise coherence and therefore the effectiveness of the current control strategy. However, even at the reduced effectiveness of 2D periodic excitation at elevated FST, it accelerated the reattachment process and the recovery rate of the reattached boundary layer, enhancing the boundary layer resistance to repeat separation and reducing its momentum loss further downstream.
Document ID
20040110909
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Ashpis, D.
(NASA Glenn Research Center Cleveland, OH, United States)
Halfon, E.
(Tel-Aviv Univ., Ramat-Aviv Tel-Aviv, Israel)
Nishri, B.
(Tel-Aviv Univ., Ramat-Aviv Tel-Aviv, Israel)
Seifert, A.
(Tel-Aviv Univ., Ramat-Aviv Tel-Aviv, Israel)
Wygnanski, I.
(Tel-Aviv Univ., Ramat-Aviv Tel-Aviv, Israel)
Date Acquired
September 7, 2013
Publication Date
August 1, 2004
Publication Information
Publication: Minnowbrook IV: 2003 Workshop on Transition and Unsteady Aspects of Turbomachinery Flows
Subject Category
Fluid Mechanics And Thermodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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