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The separated turbulent boundary layer over a wavy wallA study and application of the fourth order spline collocation procedure, numerical solution of boundary layer like differential equations, is presented. A simple inversion algorithm for the simultaneous solution of the resulting difference equations is given. Particular attention is focused on the boundary condition representation for the spline second derivative approximations. Solutions using the spline procedure, as well as the three point finite difference method, are presented for several model problems in order to assess and improve the spline numerical scheme. Application of the resulting algorithm to the incompressible laminar self similar boundary layer equations is presented.
Document ID
19780004073
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Polak, A.
(Cincinnati Univ. OH, United States)
Werle, M. J.
(Cincinnati Univ. OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-155281
Report Number: NASA-CR-155281
Accession Number
78N12016
Funding Number(s)
CONTRACT_GRANT: F33615-76-C-3091
CONTRACT_GRANT: NSG-1208
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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