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The Intermediate Wake of a Thin Flat Plate with a Circular Trailing EdgeThe intermediate wakes of thin flat plates with circular trailing edges (TEs) are investigated here with direct numerical simulations (DNSs). The separating boundary layers are turbulent in all cases. The near wake in two thin-plate cases (IN & NS), with a focus on the vortex shedding process, was explored in a recent article. Intermittent shedding was observed in Case IN. Case NS, with half the TE diameter of Case IN, was an essentially non-shedding case. A third case (ST) with a sharp trailing edge was also investigated and found to exhibit an intermittent wake instability. The objectives of the present study are twofold. The first is to determine if the wake instability found in Case ST exists in Cases IN and NS as well. The second is to provide the distributions of the turbulent normal intensities and shear stress in the wake and to understand these distributions via the budget terms in the corresponding transport equations. The results show that both Cases IN & NS exhibit a wake instability in the intermediate wake region, that is similar to that found earlier in Case ST. We note that in Case IN, the presence of an intermediate-wake instability results in the co-existence of two different types of instability within a single wake. The distributions of the turbulent normal intensities and shear stress, and the budget terms for the streamwise intensity are included and discussed here. All the budget terms contribute appreciably to the overall budget in the transport equation for streamwise normal intensity.
Document ID
20190025758
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Rai, Man Mohan
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
June 7, 2019
Publication Date
April 1, 2019
Subject Category
Aerodynamics
Report/Patent Number
ARC-E-DAA-TN67460
NASA/TM-2019-220195
Report Number: ARC-E-DAA-TN67460
Report Number: NASA/TM-2019-220195
Funding Number(s)
WBS: 106148.03.01.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
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