On the laminar region and the initial stages of transition in transitional separation bubbles
Separated transitional boundary layer flows exhibit a laminar region after separation. The momentum thickness and the distance to the wall of the separated shear layer are the key parameters controlling the instability process that promotes transition and the reattachment of the flow. This work prop...
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Published in | European journal of mechanics, B, Fluids Vol. 49; pp. 171 - 183 |
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Main Authors | , |
Format | Journal Article |
Language | English |
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Elsevier Masson SAS
01.01.2015
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ISSN | 0997-7546 1873-7390 |
DOI | 10.1016/j.euromechflu.2014.08.006 |
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Abstract | Separated transitional boundary layer flows exhibit a laminar region after separation. The momentum thickness and the distance to the wall of the separated shear layer are the key parameters controlling the instability process that promotes transition and the reattachment of the flow. This work proposes scaling laws for the defining parameters of this shear layer: its angle with the wall, its length, and the momentum thickness evolution. The laws are supported by experimental measurements performed in a boundary layer that develops over a flat plate, subject to an adverse pressure gradient such that in the inviscid limit the velocity over the plate decreases linearly along its length. The flow Reynolds number based on the characteristic boundary layer edge velocity and deceleration length takes values in the 105–106 range. The edge velocity and the momentum thickness along the separated shear layer are found to be almost constant. Furthermore, the layer is seen to separate from the wall with the appropriate angle to compensate the externally imposed adverse pressure gradient, and a relationship between its length and angle is found. Additionally, a comparison between Linear Stability Theory for parallel flows and hot-wire velocity spectral measurements performed in the separated shear layer is presented. A good agreement between the most unstable frequencies and amplification rates predicted by this theory and the ones experimentally measured is found. The hypothesis of a Kelvin–Helmholtz like instability (inviscid or inflectional instability) triggering the instability process is also reinforced as a result. |
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AbstractList | Separated transitional boundary layer flows exhibit a laminar region after separation. The momentum thickness and the distance to the wall of the separated shear layer are the key parameters controlling the instability process that promotes transition and the reattachment of the flow. This work proposes scaling laws for the defining parameters of this shear layer: its angle with the wall, its length, and the momentum thickness evolution. The laws are supported by experimental measurements performed in a boundary layer that develops over a flat plate, subject to an adverse pressure gradient such that in the inviscid limit the velocity over the plate decreases linearly along its length. The flow Reynolds number based on the characteristic boundary layer edge velocity and deceleration length takes values in the 10 super(5)-10 super(6) range. The edge velocity and the momentum thickness along the separated shear layer are found to be almost constant. Furthermore, the layer is seen to separate from the wall with the appropriate angle to compensate the externally imposed adverse pressure gradient, and a relationship between its length and angle is found. Additionally, a comparison between Linear Stability Theory for parallel flows and hot-wire velocity spectral measurements performed in the separated shear layer is presented. A good agreement between the most unstable frequencies and amplification rates predicted by this theory and the ones experimentally measured is found. The hypothesis of a Kelvin-Helmholtz like instability (inviscid or inflectional instability) triggering the instability process is also reinforced as a result. Separated transitional boundary layer flows exhibit a laminar region after separation. The momentum thickness and the distance to the wall of the separated shear layer are the key parameters controlling the instability process that promotes transition and the reattachment of the flow. This work proposes scaling laws for the defining parameters of this shear layer: its angle with the wall, its length, and the momentum thickness evolution. The laws are supported by experimental measurements performed in a boundary layer that develops over a flat plate, subject to an adverse pressure gradient such that in the inviscid limit the velocity over the plate decreases linearly along its length. The flow Reynolds number based on the characteristic boundary layer edge velocity and deceleration length takes values in the 105–106 range. The edge velocity and the momentum thickness along the separated shear layer are found to be almost constant. Furthermore, the layer is seen to separate from the wall with the appropriate angle to compensate the externally imposed adverse pressure gradient, and a relationship between its length and angle is found. Additionally, a comparison between Linear Stability Theory for parallel flows and hot-wire velocity spectral measurements performed in the separated shear layer is presented. A good agreement between the most unstable frequencies and amplification rates predicted by this theory and the ones experimentally measured is found. The hypothesis of a Kelvin–Helmholtz like instability (inviscid or inflectional instability) triggering the instability process is also reinforced as a result. |
Author | Lázaro, B.J. Serna, J. |
Author_xml | – sequence: 1 givenname: J. orcidid: 0000-0001-5593-6330 surname: Serna fullname: Serna, J. email: jose.serna@cud.upct.es, jsernaser@gmail.com organization: School of Aeronautics, Universidad Politécnica de Madrid, 28040 Madrid, Spain – sequence: 2 givenname: B.J. surname: Lázaro fullname: Lázaro, B.J. organization: School of Aeronautics, Universidad Politécnica de Madrid, 28040 Madrid, Spain |
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CitedBy_id | crossref_primary_10_1016_j_piutam_2015_03_078 crossref_primary_10_1016_j_ast_2014_10_010 crossref_primary_10_1007_s10665_021_10125_3 crossref_primary_10_1063_1_5122889 crossref_primary_10_2514_1_J056567 crossref_primary_10_1016_j_jppr_2018_12_004 crossref_primary_10_1002_pamm_201710282 |
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SubjectTerms | Boundary layer Fluid dynamics Fluid flow Hydrodynamic stability Instability Separation Separation bubble Shear layers Stability Walls |
Title | On the laminar region and the initial stages of transition in transitional separation bubbles |
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