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Large Eddy Simulation in a Channel with Exit Boundary ConditionsThe influence of the exit boundary conditions (vanishing first derivative of the velocity components and constant pressure) on the large eddy simulation of the fully developed turbulent channel flow has been investigated for equidistant and stretched grids at the channel exit. Results show that the chosen exit boundary conditions introduce some small disturbance which is mostly damped by the grid stretching. The difference between the fully developed turbulent channel flow obtained with LES with periodicity condition and the inlet and exit and the LES with fully developed flow at the inlet and the exit boundary condition is less than 10% for equidistant grids and less than 5% for the case grid stretching. The chosen boundary condition is of interest because it may be used in complex flows with backflow at exit.
Document ID
19960020945
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Cziesla, T.
(Ruhr Univ. Bochum, Germany)
Braun, H.
(Ruhr Univ. Bochum, Germany)
Biswas, G.
(Indian Inst. of Tech. Kanpur, India)
Mitra, N. K.
(Institute for Computer Applications in Science and Engineering Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:198304
NASA-CR-198304
ICASE-96-18
Report Number: NAS 1.26:198304
Report Number: NASA-CR-198304
Report Number: ICASE-96-18
Accession Number
96N24458
Funding Number(s)
PROJECT: RTOP 505-90-52-01
CONTRACT_GRANT: NAS1-19480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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