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Mechanisms of Stationary Crossflow Instability Growth and Breakdown Induced by Forward-Facing Steps An experimental study is performed to determine the mechanisms by which a forward-facing step impacts the growth and breakdown to turbulence of the stationary cross-flow instability. Particle image velocimetry measurements are obtained in the boundary layer of a 30◦swept flat plate with a pressure body. Step heights range from 53 % to 71 % of the boundary-layer thickness. The critical step height is approximately 60 % of the boundary-layer thickness for the current study, although it is also shown that the critical step height depends on the initial amplitude of the stationary cross-flow vortices. For the critical cases, the stationary cross-flow amplitude grows sharply downstream of the step, decays for a short region and then grows again. The initial growth region is linear, and can be explained primarily through the impact of the step on the mean flow. Namely, the step causes abrupt changes to the mean flow, resulting in large values of wall-normal shear, as well as highly inflectional profiles, due to either cross-flow reversal, separation or both. These inflectional profiles are highly unstable for the stationary cross-flow. Additionally,the reversed flow regions are significantly modulated by the stationary cross-flow vortices. The second region of growth occurs due to the stationary-cross-flow-induced modulation of the shear layer, which leads to multiple smaller wavelength stream wise vortices. High-frequency fluctuations indicate that the unsteady transition mechanism for the critical cases relates to the shedding of vortices downstream of reattachment of the modulated separated regions.
Document ID
20205003053
Acquisition Source
Langley Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Jenna L. Eppink ORCID
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
June 2, 2020
Publication Date
June 11, 2020
Publication Information
Publication: Journal of Fluid Mechanics
Publisher: Cambridge University Press
Volume: 897
Issue Publication Date: August 25, 2020
ISSN: 0022-1120
e-ISSN: 1469-7645
Subject Category
Aircraft Propulsion And Power
Funding Number(s)
WBS: 109492.02.07.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Professional Review
Keywords
boundary layer stability
transition to turbulence
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