Shehzad, Muhammad and Sun, Bihai and Jovic, Daniel and Atkinson, Callum and Soria, Julio and Ostovan, Yasar and Cuvier, Christophe and Foucaut, Jean Marc and Willert, Christian (2022) Effect of streamwise domain size on the POD mode characteristics in an adverse pressure gradient turbulent boundary layer. In: 12th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2022. 12th International Symposium on Turbulence and Shear Flow Phenomena (TSFP12), 2022-07-19 - 2022-07-22, Osaka, Japan.
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Official URL: http://www.tsfp-conference.org/proceedings/proceedings-of-tsfp-12-2022-osaka.html
Abstract
Proper orthogonal decomposition (POD) is used to study coherent structures on measurements of wall-bounded turbulent flows. In order to apply POD in the study of turbulent boundary layers, it is important to determine the appropriate size of the flow domain to be used in POD analysis. This study uses the 2C-2D PIV measurements of an adverse pressure gradient (APG) turbulent boundary layer (TBL) with beta ~ 0 - 3.74 and Re_delta2 ~ 1720 - 23430 where Re_delta2 is the momentum thickness based Reynolds number and beta is the Clauser's pressure gradient parameter. The measurements were obtained in the Laboratoire de Mecanique des Fluides de Lille (LMFL) High-Reynolds-Number (HRN) Boundary Layer Wind Tunnel, Lille, France. Spanning over 20 delta along the streamwise direction (where delta is the boundary layer thickness in the middle of the field of view), these are appropriate to be used in the study of the extent of the large-scale motions. POD analysis on the variable domain size along the streamwise direction (delta x) suggests that the POD mode shape changes with delta x. In this particular TBL, the shape of the first mode which represents the largest scales in the fluid flow, changes until delta x is equal to or greater than 8 delta. It is also observed the smaller scales of higher-order POD modes take longer delta x to converge in the mode shape. The streamwise integral-length-scale of 6.68 delta also confirms the size of the largest scales to be around 8 delta. Therefore, for this particular TBL, a minimum streamwise domain size of 8 delta is appropriate for the analysis of large-scale motions using POD.
| Item URL in elib: | https://elib.dlr.de/191029/ | ||||||||||||||||||||||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||||||||||||||||||||||||
| Title: | Effect of streamwise domain size on the POD mode characteristics in an adverse pressure gradient turbulent boundary layer | ||||||||||||||||||||||||||||||||||||||||
| Authors: |
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| Date: | 19 July 2022 | ||||||||||||||||||||||||||||||||||||||||
| Journal or Publication Title: | 12th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2022 | ||||||||||||||||||||||||||||||||||||||||
| Refereed publication: | No | ||||||||||||||||||||||||||||||||||||||||
| Open Access: | Yes | ||||||||||||||||||||||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||||||||||||||||||||||
| Keywords: | turbulent boundary layers, high resolution PIV, proper orthogonal decomposition | ||||||||||||||||||||||||||||||||||||||||
| Event Title: | 12th International Symposium on Turbulence and Shear Flow Phenomena (TSFP12) | ||||||||||||||||||||||||||||||||||||||||
| Event Location: | Osaka, Japan | ||||||||||||||||||||||||||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||||||||||||||||||||||||||
| Event Start Date: | 19 July 2022 | ||||||||||||||||||||||||||||||||||||||||
| Event End Date: | 22 July 2022 | ||||||||||||||||||||||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||||||||||||||||||||||
| HGF - Program Themes: | Clean Propulsion | ||||||||||||||||||||||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||||||||||||||||||||||
| DLR - Program: | L CP - Clean Propulsion | ||||||||||||||||||||||||||||||||||||||||
| DLR - Research theme (Project): | L - Virtual Engine | ||||||||||||||||||||||||||||||||||||||||
| Location: | Köln-Porz | ||||||||||||||||||||||||||||||||||||||||
| Institutes and Institutions: | Institute of Propulsion Technology > Engine Measurement Systems | ||||||||||||||||||||||||||||||||||||||||
| Deposited By: | Willert, Dr.phil. Christian | ||||||||||||||||||||||||||||||||||||||||
| Deposited On: | 02 Dec 2022 11:21 | ||||||||||||||||||||||||||||||||||||||||
| Last Modified: | 13 Nov 2024 15:12 |
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