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Large eddy simulation of turbulent channel flow: ILLIAC 4 calculationThe three-dimensional time dependent equations of motion were numerically integrated for fully-developed turbulent channel flow. A large scale flow field was obtained directly from the solution of these equations, and small scale field motions were simulated through an eddy viscosity model. The calculations were carried out on the ILLIAC 4 computer. The computed flow patterns show that the wall layer consists of coherent structures of low speed and high speed streaks alternating in the spanwise direction. These structures were absent in the regions away from the wall. Hot spots, small localized regions of very large turbulent shear stress, were frequently observed. The profiles of the pressure velocity-gradient correlations show a significant transfer of energy from the normal to the spanwise component of turbulent kinetic energy in the immediate neighborhood of the wall ('the splatting effect').
Document ID
19790023981
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kim, J.
(NASA Ames Research Center Moffett Field, CA, United States)
Moin, P.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1979
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-TM-78619
A-7952
Meeting Information
Meeting: AGARD Symp. on Turbulent Boundary Layer, Experiment, Theory, and Modelling
Location: The Hague
Country: Netherlands
Start Date: September 24, 1979
End Date: September 27, 1979
Accession Number
79N32152
Funding Number(s)
PROJECT: RTOP 506-26-11-07-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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