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Numerical simulations of the nonlinear kink modes in linearly stable supersonic slip surfacesHigh-resolution numerical simulations of supersonic slip surfaces were performed using the Cray 2 at the Minnesota Supercomputer Center to confirm earlier analytic nonlinear stability calculations of such structures. The present study presents a numerical solution for the problem solved analytically by Artola and Majda (1987) and follows growing modes well into the large-amplitude regime. The response of an equal-density Mach-4 slip surface to a variety of impinging nonlinear sound wave trains is computed using the piecewise-parabolic method (PPM). The nature of the nonlinear kink modes observed in the simulations was found to be similar to that discussed by Artola and Majda. Most of the speeds moved in either direction, with speeds near the predicted value. It is suggested that the stationary modes will eventually dominate the flow at much later times, and it is argued that the stationary modes are more disruptive than the propagating kink modes.
Document ID
19910055105
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Pedelty, Jeffrey A.
(NASA Goddard Space Flight Center Greenbelt, MD; Minnesota, University, Minneapolis, United States)
Woodward, Paul R.
(Minnesota, University Minneapolis, United States)
Date Acquired
August 15, 2013
Publication Date
April 1, 1991
Publication Information
Publication: Journal of Fluid Mechanics
Volume: 225
ISSN: 0022-1120
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
91A39728
Funding Number(s)
CONTRACT_GRANT: DE-FG02-87ER-25035
CONTRACT_GRANT: AF-AFOSR-86-0239
CONTRACT_GRANT: NSF AST-86-11404
CONTRACT_GRANT: NSF AST-83-15949
Distribution Limits
Public
Copyright
Other

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