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Generalized Wall Function for Complex Turbulent FlowsA generalized wall function was proposed by Shih et al., (1999). It accounts the effect of pressure gradients on the flow near the wall. Theory shows that the effect of pressure gradients on the flow in the inertial sublayer is very significant and the standard wall function should be replaced by a generalized wall function. Since the theory is also valid for boundary layer flows toward separation, the generalized wall function may be applied to complex turbulent flows with acceleration, deceleration, separation and recirculation. This paper is to verify the generalized wall function with numerical simulations for boundary layer flows with various adverse and favorable pressure gradients, including flows about to separate. Furthermore, a general procedure of implementation of the generalized wall function for National Combustion Code (NCC) is described, it can be applied to both structured and unstructured CFD codes.
Document ID
20000063378
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Shih, Tsan-Hsing
(NASA Glenn Research Center Cleveland, OH United States)
Povinelli, Louis A.
(NASA Glenn Research Center Cleveland, OH United States)
Liu, Nan-Suey
(NASA Glenn Research Center Cleveland, OH United States)
Chen, Kuo-Huey
(Toledo Univ. OH United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2000
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:209936
NASA/TM-2000-209936
ICOMP-2000-04
E-12182
Report Number: NAS 1.15:209936
Report Number: NASA/TM-2000-209936
Report Number: ICOMP-2000-04
Report Number: E-12182
Meeting Information
Meeting: Aerospace Sciences
Location: Reno, NV
Country: United States
Start Date: January 10, 2000
End Date: January 13, 2000
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 522-31-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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