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Correlation-based Transition Modeling for Three-dimensional Aerodynamic Configurations

Grabe, Cornelia and Krumbein, Andreas (2014) Correlation-based Transition Modeling for Three-dimensional Aerodynamic Configurations. 6th European Conference on Computational Fluid Dynamics, 20. - 25. July 2014, Barcelona, Spanien.

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Official URL: http://www.wccm-eccm-ecfd2014.org/admin/files/fileabstract/a1674.pdf


The prediction of boundary-layer transition is an important element of airfoil and wing design as the correct prediction of transition locations influences the resulting lift and drag forces and, thus, the overall performance. Boundary-layer transition is characterized by boundary-layer quantities like the velocity profiles in the boundary layer along a streamline or the momentum thickness computed from these profiles. In Computational Fluid Dynamics (CFD), many codes are based on the finite-volume discretization of the Reynolds Averaged Navier-Stokes (RANS) equations. Computations with these codes yield no information about streamlines in the flow, which means the characterizing quantities for boundary-layer transition are not directly available. To deal with this, two different approaches were introduced into the DLR TAU code, the unstructured CFD solver of DLR for aircraft analysis and design.

Item URL in elib:https://elib.dlr.de/92011/
Document Type:Conference or Workshop Item (Speech)
Title:Correlation-based Transition Modeling for Three-dimensional Aerodynamic Configurations
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Page Range:pp. 1-2
Series Name:Conference proceedings online, e-book
Keywords:Boundary-layer Transition, Correlation-based Transition model, Three-dimensional configuration
Event Title:6th European Conference on Computational Fluid Dynamics
Event Location:Barcelona, Spanien
Event Type:international Conference
Event Dates:20. - 25. July 2014
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Deposited By: Micknaus, Ilka
Deposited On:21 Nov 2014 09:57
Last Modified:21 Nov 2014 09:57

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