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On the low-frequency dynamics of turbulent separation bubbles
Tech Univ Berlin, Inst Luft & Raumfahrt, D-10587 Berlin, Germany..
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, School of Engineering Sciences (SCI), Engineering Mechanics.ORCID iD: 0000-0002-5913-5431
Inst Tecnol Aeronaut, Div Engn Aeronaut, Sao Jose Dos Campos, SP, Brazil..
Tech Univ Berlin, Inst Luft & Raumfahrt, D-10587 Berlin, Germany..
2024 (English)In: Journal of Fluid Mechanics, ISSN 0022-1120, E-ISSN 1469-7645, Vol. 991, article id A11Article in journal (Refereed) Published
Abstract [en]

The low-frequency modal and non-modal linear dynamics of an incompressible, pressure-gradient-induced turbulent separation bubble (TSB) are investigated, with the objective of studying the mechanism responsible for the low-frequency contraction and expansion (breathing) commonly observed in experimental studies. The configuration of interest is a TSB generated on a flat test surface by a succession of adverse and favourable pressure gradients. The base flow selected for the analysis is the average TSB from the direct numerical simulation of Coleman et al. (J. Fluid Mech., vol. 847, 2018, pp. 28-70). Global mode analysis reveals that the eigenmodes of the linear operator are damped for all frequencies and wavenumbers. Furthermore, the least damped eigenmode appears to occur at zero frequency and low, non-zero spanwise wavenumber when scaled with the separation length. Resolvent analysis is then employed to examine the forced dynamics of the flow. At low frequency, a region of low, non-zero spanwise wavenumber is also discernible, where the receptivity appears to be driven by the identified weakly damped global mode. The corresponding optimal energy gain is shown to have the shape of a first-order, low-pass filter with a cut-off frequency consistent with the low-frequency unsteadiness in TSBs. The results from resolvent analysis are compared to the unsteady experimental database of Le Floc'h et al. (J. Fluid Mech., vol. 902, 2020, A13) in a similar TSB flow. The alignment between the optimal response and the first spectral proper orthogonal decomposition mode computed from the experiments is shown to be close to 95%, while the spanwise wavenumber of the optimal response is consistent with that of the low-frequency breathing motion captured experimentally. This indicates that the fluctuations observed experimentally at low frequency closely match the response computed from resolvent analysis. Based on these results, we propose that the forced dynamics of the flow, driven by the weakly damped global mode, serve as a plausible mechanism for the origin of the low-frequency breathing motion commonly observed in experimental studies of TSBs.

Place, publisher, year, edition, pages
Cambridge University Press (CUP) , 2024. Vol. 991, article id A11
Keywords [en]
boundary layer separation, separated flows
National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-352732DOI: 10.1017/jfm.2024.532ISI: 001294826600001Scopus ID: 2-s2.0-85201917955OAI: oai:DiVA.org:kth-352732DiVA, id: diva2:1895340
Note

QC 20240905

Available from: 2024-09-05 Created: 2024-09-05 Last updated: 2025-02-09Bibliographically approved

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Hanifi, Ardeshir

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