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Towards a Viscous Wall Model for Immersed Boundary Methods

Authors :
Christoph Brehm
Michael F. Barad
Cetin C. Kiris
Source :
2018 AIAA Aerospace Sciences Meeting.
Publication Year :
2018
Publisher :
American Institute of Aeronautics and Astronautics, 2018.

Abstract

Immersed boundary methods are frequently employed for simulating flows at low Reynolds numbers or for applications where viscous boundary layer effects can be neglected. The primary shortcoming of Cartesian mesh immersed boundary methods is the inability of efficiently resolving thin turbulent boundary layers in high-Reynolds number flow application. The inefficiency of resolving the thin boundary is associated with the use of constant aspect ratio Cartesian grid cells. Conventional CFD approaches can efficiently resolve the large wall normal gradients by utilizing large aspect ratio cells near the wall. This paper presents different approaches for immersed boundary methods to account for the viscous boundary layer interaction with the flow-field away from the walls. Different wall modeling approaches proposed in previous research studies are addressed and compared to a new integral boundary layer based approach. In contrast to common wall-modeling approaches that usually only utilize local flow information, the integral boundary layer based approach keeps the streamwise history of the boundary layer. This allows the method to remain effective at much larger y+ values than local wall modeling approaches. After a theoretical discussion of the different approaches, the method is applied to increasingly more challenging flow fields including fully attached, separated, and shock-induced separated (laminar and turbulent) flows.

Details

Database :
OpenAIRE
Journal :
2018 AIAA Aerospace Sciences Meeting
Accession number :
edsair.doi...........f9bd451bc1d97bc07dad4757f2b7c195