Esther Lagemann, Julia Roeb, Steven L. Brunton, Christian Lagemann
{"title":"A deep learning approach to wall-shear stress quantification: From numerical training to zero-shot experimental application","authors":"Esther Lagemann, Julia Roeb, Steven L. Brunton, Christian Lagemann","doi":"arxiv-2409.03933","DOIUrl":null,"url":null,"abstract":"The accurate quantification of wall-shear stress dynamics is of substantial\nimportance for various applications in fundamental and applied research,\nspanning areas from human health to aircraft design and optimization. Despite\nsignificant progress in experimental measurement techniques and post-processing\nalgorithms, temporally resolved wall-shear stress dynamics with adequate\nspatial resolution and within a suitable spatial domain remain an elusive goal.\nTo address this gap, we introduce a deep learning architecture that ingests\nwall-parallel velocity fields from the logarithmic layer of turbulent\nwall-bounded flows and outputs the corresponding 2D wall-shear stress fields\nwith identical spatial resolution and domain size. From a physical perspective,\nour framework acts as a surrogate model encapsulating the various mechanisms\nthrough which highly energetic outer-layer flow structures influence the\ngoverning wall-shear stress dynamics. The network is trained in a supervised\nfashion on a unified dataset comprising direct numerical simulations of\nstatistically 1D turbulent channel and spatially developing turbulent boundary\nlayer flows at friction Reynolds numbers ranging from 390 to 1,500. We\ndemonstrate a zero-shot applicability to experimental velocity fields obtained\nfrom Particle-Image Velocimetry measurements and verify the physical accuracy\nof the wall-shear stress estimates with synchronized wall-shear stress\nmeasurements using the Micro-Pillar Shear-Stress Sensor for Reynolds numbers up\nto 2,000. In summary, the presented framework lays the groundwork for\nextracting inaccessible experimental wall-shear stress information from readily\navailable velocity measurements and thus, facilitates advancements in a variety\nof experimental applications.","PeriodicalId":501125,"journal":{"name":"arXiv - PHYS - Fluid Dynamics","volume":"1 1","pages":""},"PeriodicalIF":0.0000,"publicationDate":"2024-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"arXiv - PHYS - Fluid Dynamics","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/arxiv-2409.03933","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
The accurate quantification of wall-shear stress dynamics is of substantial
importance for various applications in fundamental and applied research,
spanning areas from human health to aircraft design and optimization. Despite
significant progress in experimental measurement techniques and post-processing
algorithms, temporally resolved wall-shear stress dynamics with adequate
spatial resolution and within a suitable spatial domain remain an elusive goal.
To address this gap, we introduce a deep learning architecture that ingests
wall-parallel velocity fields from the logarithmic layer of turbulent
wall-bounded flows and outputs the corresponding 2D wall-shear stress fields
with identical spatial resolution and domain size. From a physical perspective,
our framework acts as a surrogate model encapsulating the various mechanisms
through which highly energetic outer-layer flow structures influence the
governing wall-shear stress dynamics. The network is trained in a supervised
fashion on a unified dataset comprising direct numerical simulations of
statistically 1D turbulent channel and spatially developing turbulent boundary
layer flows at friction Reynolds numbers ranging from 390 to 1,500. We
demonstrate a zero-shot applicability to experimental velocity fields obtained
from Particle-Image Velocimetry measurements and verify the physical accuracy
of the wall-shear stress estimates with synchronized wall-shear stress
measurements using the Micro-Pillar Shear-Stress Sensor for Reynolds numbers up
to 2,000. In summary, the presented framework lays the groundwork for
extracting inaccessible experimental wall-shear stress information from readily
available velocity measurements and thus, facilitates advancements in a variety
of experimental applications.