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On the modulational instability of large amplitude waves in supersonic boundary layersThe evolution of large amplitude Tollmien-Schlichting waves in a supersonic boundary layer is investigated. Disturbances which have their wavenumber and frequency slowly varying in time and space are described using a phase equation type of approach. Unlike the incompressible case we find that the initial bifurcation to a finite amplitude Tollmien-Schlichting wave is subcritical for most Mach numbers. In fact the bifurcation is only supercritical for a small range of Mach numbers and even then for only a finite range of wave propagation angles. The modulational instability of large amplitude wavetrains is considered and is shown to be governed by an equation similar to Burgers equation but with the viscous term replaced by a fractional derivative. A numerical investigation of the solution of this equation is described. It is shown that uniform wavetrains are unstable.
Document ID
19950021339
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Hall, Philip
(Manchester Univ. United Kingdom)
Papageorgiou, Demetrios T.
(New Jersey Inst. of Tech. Newark, NJ., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ICASE-95-29
NASA-CR-195072
NAS 1.26:195072
Report Number: ICASE-95-29
Report Number: NASA-CR-195072
Report Number: NAS 1.26:195072
Accession Number
95N27760
Funding Number(s)
CONTRACT_GRANT: F49620-94-1-0242
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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