NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Free-stream disturbance, continuous Eigenfunctions, boundary-layer instability and transitionA rational foundation is presented for the application of the linear shear flows to transition prediction, and an explicit method is given for carrying out the necessary calculations. The expansions used are shown to be complete. Sample calculations show that a typical boundary layer is very sensitive to vorticity disturbances 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 Tollmien-Schlicting waves are an extremely small fraction of the amplitude of the disturbance.
Document ID
19810001814
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Grosch, C. E.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1980
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-163669
Report Number: NASA-CR-163669
Accession Number
81N10322
Funding Number(s)
CONTRACT_GRANT: NSG-1618
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available