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A nonlinear investigation of the stationary modes of instability of the three-dimensional compressible boundary layer due to a rotating discThe effects of compressibility on a stationary mode of instability of the 3-D boundary layer due to a rotating disc are investigated. The aim is to determine whether this mode will be important in the finite amplitude destabilization of the boundary layer. This stationary mode is characterized by the effective velocity profile having zero shear stress at the wall. Triple-deck solutions are presented for an adiabatic wall and an isothermal wall. It is found that this stationary mode is only possible over a finite range of Mach numbers. Asymptotic solutions are obtained which describe the structure of the wavenumber and the orientation of these modes as functions of the local Mach number. The effects of nonlinearity are investigated allowing the finite amplitude growth of a disturbance close to the neutral location to be described.
Document ID
19890019395
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Seddougui, Sharon O.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-181901
NAS 1.26:181901
ICASE-89-50
Report Number: NASA-CR-181901
Report Number: NAS 1.26:181901
Report Number: ICASE-89-50
Accession Number
89N28766
Funding Number(s)
PROJECT: RTOP 505-90-21-01
CONTRACT_GRANT: NAS1-18605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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