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Development of perturbations in the boundary layerThe transition of laminar flows into turbulent flows in a boundary layer is discussed. The individual aspects of the transition process, observed under controllable model conditions are examined. The aspect of this problem, namely the development or excitation of the natural oscillations in the boundary layer, the so-called Tollmin-Schlichting waves is covered. Three types of excitation of these waves are considered: (1) distributed generation throughout the boundary layer; (2) generation in the vicinity of the forward edge of a model, having either a sharp edge or an edge with a large radius or curvature, and (3) generation in a developed boundary layer by means of a focused effect.
Document ID
19860012322
Acquisition Source
Legacy CDMS
Document Type
Book
Authors
Dovgal, A. V.
(NASA Headquarters Washington, DC United States)
Kachanov, Y. S.
(NASA Headquarters Washington, DC United States)
Kozlov, V. V.
(NASA Headquarters Washington, DC United States)
Levchenko, V. Y.
(NASA Headquarters Washington, DC United States)
Maksimov, V. P.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1986
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-77986
NAS 1.15:77986
Report Number: NASA-TM-77986
Report Number: NAS 1.15:77986
Accession Number
86N21793
Funding Number(s)
CONTRACT_GRANT: NASW-4005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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