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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 spectral method with up to about 10 to the 7th grid points. Periodic spanwise and streamwise 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 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
19880041667
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Spalart, Philippe R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
February 1, 1988
Publication Information
Publication: Journal of Fluid Mechanics
Volume: 187
ISSN: 0022-1120
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ISSN: 0022-1120
Accession Number
88A28894
Distribution Limits
Public
Copyright
Other

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