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Wave interactions in a three-dimensional attachment-line boundary layerThe three-dimensional boundary layer on a swept wing can support different types of hydrodynamic instability. Here attention is focused on the so-called 'spanwise instability' problem which occurs when the attachment-line boundary layer on the leading edge becomes unstable to Tollmien-Schlichting waves. In order to gain insight into the interactions that are important in that problem a simplified basic state is considered. This simplified flow corresponds to the swept attachemnt-line boundary layer on an infinite flat plate. The basic flow here is an exact solution of the Navier-Stokes equations and its stability to two-dimensional waves propagating along the attachment line can be considered exactly at finite Reynolds number. The corresponding problem is studied for oblique waves, and their interaction with two-dimensional waves is investigated. It is shown that there are two types of oblique wave which, if excited, cause the destabilization of the two-dimensional mode and the breakdown of the disturbed flow at a finite distance from the leading edge.
Document ID
19900061660
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hall, Philip
(Exeter University United Kingdom)
Seddougui, Sharon O.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
August 1, 1990
Publication Information
Publication: Journal of Fluid Mechanics
Volume: 217
ISSN: 0022-1120
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0022-1120
Accession Number
90A48715
Funding Number(s)
CONTRACT_GRANT: NAS1-18107
Distribution Limits
Public
Copyright
Other

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