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Direct simulation of a turbulent boundary layer up to R(sub)(theta)= 1410The turbulent boundary layer on a flat plate, with zero pressure gradient, is simulated numerically at four stations between R sub theta = 225 and R sub theta = 1410. The three-dimensional time-dependent Navier-Stokes equations are solved using a spectra method with up to about 10 to the 7th power grid points. Periodic spanwise and stream-wise conditions are applied, and a multiple-scale procedure is applied to approximate the slow streamwise growth of the boundary layer. The flow is studied, primarily, from a statistical point of view. The solutions are compared with experimental results. The scaling of the mean and turbulent quantities with Reynolds number is examined and compared with accepted laws, and the significant deviations are documented. The turbulence at the highest Reynolds number is studied in detail. The spectra are compared with various theoretical models. Reynolds-stress budget data are provided for turbulence-model testing.
Document ID
19870008597
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Spalart, Philippe R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1986
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-89407
A-87016
NAS 1.15:89407
Report Number: NASA-TM-89407
Report Number: A-87016
Report Number: NAS 1.15:89407
Accession Number
87N18030
Funding Number(s)
PROJECT: RTOP 505-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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