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Forward marching procedure for separated boundary-layer flowsA forward-marching procedure for separated boundary-layer flows which permits the rapid and accurate solution of flows of limited extent is presented. The streamwise convection of vorticity in the reversed flow region is neglected, and this approximation is incorporated into a previously developed (Carter, 1974) inverse boundary-layer procedure. The equations are solved by the Crank-Nicolson finite-difference scheme in which column iteration is carried out at each streamwise station. Instabilities encountered in the column iterations are removed by introducing timelike terms in the finite-difference equations. This provides both unconditional diagonal dominance and a column iterative scheme, found to be stable using the von Neumann stability analysis.
Document ID
19760031018
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Carter, J. E.
(NASA Langley Research Center Hampton, VA, United States)
Wornom, S. F.
(NASA Langley Research Center Subsonic and Transonic Aerodynamics Div., Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: AIAA Journal
Volume: 13
Subject Category
Aerodynamics
Accession Number
76A13984
Distribution Limits
Public
Copyright
Other

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