NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Numerical simulation of boundary layers. Part 3: Turbulence and relaminarization in sink flowsDirect numerical simulations of sink-flow boundary layers, with acceleration parameters K between 1.5 and 3.0 x 10 to the -6 power, are presented. The three-dimensional, time-dependent Navier-Stokes equations are solved numerically using a spectral method, with about 10 to the -6 degrees of freedom. The flow is assumed to be statistically steady, and self-similar. A multiple-scale approximation and periodic conditions are applied to the fluctuations. The turbulence is studied using instantaneous and statistical results. Good agreement with the experiments of Jones and Launder is observed. Two effects of the favorable pressure gradient are to extend the logarithmic layer, and to alter the energy balance of the turbulence near the edge of the boundary layer. At very low Reynolds number the logarithmic layer is shortened and slightly displaced, but wall-layer streaks are present even at the lowest values of the Reynolds number for which turbulence can be sustained. Large quiescent patches appear in the flow. Relaminarization occurs at K = 3.0 x 10 to the -6 power, corresponding to a Reynolds number, based on momentum thickness, of about 330.
Document ID
19880004901
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Spalart, Philippe R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1986
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-88220
A-86073
NAS 1.15:88220
Accession Number
88N14283
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available