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The initial-value problem for viscous channel flowsPlane viscous channel flows are perturbed and the ensuing initial-value problems are investigated in detail. Unlike traditional methods where traveling wave normal modes are assumed for solution, this works offers a means whereby completely arbitrary initial input can be specified without having to resort to eigenfunction expansions. The full temporal behavior, including both early time transients and the long time asymptotics, can be determined for any initial disturbance. Effects of three-dimensionality can be assessed. The bases for the analysis are: (a) linearization of the governing equations; (b) Fourier decomposition in the spanwise and streamwise directions of the flow; and (c) direct numerical integration of the resulting partial differential equations. All of the stability data that are known for such flows can be reproduced. Also, the optimal initial condition can be determined in a straight forward manner and such optimal conditions clearly reflect transient growth data that is easily determined by a rational choice of a basis for the initial conditions. Although there can be significant transient growth for subcritical values of the Reynolds number using this approach it does not appear possible that arbitrary initial conditions will lead to the exceptionally large transient amplitudes that have been determined by optimization of normal modes. The approach is general and can be applied to other classes of problems where only a finite discrete spectrum exists, such as the boundary layer for example.
Document ID
19950016790
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Criminale, W. O.
(Washington Univ. Seattle, WA., United States)
Jackson, T. L.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Lasseigne, D. G.
(Old Dominion Univ. Norfolk, VA., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICASE-95-6
NAS 1.26:195034
NASA-CR-195034
Report Number: ICASE-95-6
Report Number: NAS 1.26:195034
Report Number: NASA-CR-195034
Accession Number
95N23207
Funding Number(s)
CONTRACT_GRANT: NAS1-19480
PROJECT: RTOP 505-90-52-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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