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Inverse solutions for laminar boundary-layer flows with separation and reattachmentNumerical solutions of the laminar, incompressible boundary layer equations are presented for flows involving separation and reattachment. Regular solutions are obtained with an inverse approach in which either the displacement thickness or the skin friction is specified; the pressure is deduced from the solution. A vorticity-stream-function formulation of the boundary layer equations is used to eliminate the unknown pressure. Solutions of the resulting finite difference equations, in which the flow direction is taken into account, are obtained by several global iteration schemes which are stable and have unconditional diagonal dominance. Results are compared with Klineberg and Steger's separated boundary layer calculations, and with Briley's solution of Navier-Stokes equations for a separated region. In addition, an approximate technique is presented in which the streamwise convection of vorticity is set equal to zero in the reversed flow region; such a technique results in a quick forward marching procedure for separated flows.
Document ID
19760004927
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Carter, J. E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
L-10336
NASA-TR-R-447
Report Number: L-10336
Report Number: NASA-TR-R-447
Accession Number
76N12015
Funding Number(s)
PROJECT: RTOP 505-06-31-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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