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Free-stream disturbances, continuous eigenfunctions, boundary-layer instability and transitionA rational foundation is provided for the application of the linear stability theory of parallel shear flows to transition prediction. An explicit method is given for carrying out the necessary calculations. The expansions are shown to be complete. Sample calculations show that a typical boundary layer is very sensitive to vorticity disturbance in the inner boundary layer near the critical layer. Vorticity disturbances three or four boundary layer thicknesses above the boundary are nearly uncoupled from the boundary layer, in that the amplitudes of the discrete Tollmein-Schlichting waves are an extremely small fraction of the amplitude of the disturbance.
Document ID
19810005754
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Salwen, H.
(Stevens Inst. of Tech. Hoboken, NJ, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1980
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-163828
Report Number: NASA-CR-163828
Accession Number
81N14266
Funding Number(s)
CONTRACT_GRANT: NSG-1619
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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