NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Towards a Viscous Wall Model for Immersed Boundary MethodsImmersed 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.
Document ID
20160011719
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Brehm, Christoph
(Arizona Univ. Tucson, AZ, United States)
Barad, Michael F.
(NASA Ames Research Center Moffett Field, CA United States)
Kiris, Cetin C.
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
October 3, 2016
Publication Date
June 13, 2016
Subject Category
Aeronautics (General)
Numerical Analysis
Report/Patent Number
ARC-E-DAA-TN28643
Report Number: ARC-E-DAA-TN28643
Meeting Information
Meeting: AIAA Fluid Dynamics Conference
Location: Washington, D.C.
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNX15AW29G
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Immersed
Viscous
Bondary Method
No Preview Available