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Numerical simulation of two-dimensional spatially-developing mixing layersTwo-dimensional, incompressible, spatially developing mixing layer simulations are performed at Re = 10(exp 2) and 10(exp 4) with two classes of perturbations applied at the inlet boundary; combinations of discrete modes from linear stability theory, and a broad spectrum of modes derived from experimentally measured velocity spectra. The effect of the type and strength of inlet perturbations on vortex dynamics and time-averaged properties are explored. Two-point spatial velocity and autocorrelations are used to estimate the size and lifetime of the resulting coherent structures and to explore possible feedback effects. The computed time-averaged properties such as mean velocity profiles, turbulent statistics, and spread rates show good agreement with experimentally measured values. It is shown that by forcing with a broad spectrum of modes derived from an experimental energy spectrum many experimentally observed phenomena can be reproduced by a 2-D simulation. The strength of the forcing merely affected the length required for the dominant coherent structures to become fully-developed. Thus intensities comparable to those of the background turbulence in many wind tunnel experiments produced the same results, given sufficient simulation length.
Document ID
19940030180
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wilson, R. V.
(Old Dominion Univ. Norfolk, VA., United States)
Demuren, A. O.
(Old Dominion Univ. Norfolk, VA., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AD-A281683
NASA-CR-194911
NAS 1.26:194911
ICASE-94-32
Report Number: AD-A281683
Report Number: NASA-CR-194911
Report Number: NAS 1.26:194911
Report Number: ICASE-94-32
Accession Number
94N34686
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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