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Changes in Flat Plate Wake Characteristics Obtained With Decreasing Plate ThicknessThe near and very near wake of a flat plate with a circular trailing edge is investigated with data from direct numerical simulations. Computations were performed for four different Reynolds numbers based on plate thickness (D) and at constant plate length. The value of θ/D varies by a factor of approximately 20 in the computations (θ being the boundary layer momentum thickness at the trailing edge). The separating boundary layers are turbulent in all the cases. One objective of the study is to understand the changes in wake characteristics as the plate thickness is reduced (increasing θ/D). Vortex shedding is vigorous in the low θ/D cases with a substantial decrease in shedding intensity in the largest θ/D case (for all practical purposes shedding becomes almost intermittent). Other characteristics that are significantly altered with increasing θ/D are the roll-up of the detached shear layers and the magnitude of fluctuations in shedding period. These effects are explored in depth. The effects of changing θ/D on the distributions of the time-averaged, near-wake velocity statistics are discussed.
Document ID
20160010448
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
August 19, 2016
Publication Date
July 1, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Physics (General)
Aeronautics (General)
Report/Patent Number
NASA/TM-2016-219142
ARC-E-DAA-TN34014
Report Number: NASA/TM-2016-219142
Report Number: ARC-E-DAA-TN34014
Funding Number(s)
WBS: WBS 106148.03.01.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Wakes
CFD
Turbulence
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