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Solutions for incompressible separated boundary layers including viscous-inviscid interactionNumerical solutions are presented for the laminar and turbulent boundary-layer equations for incompressible flows with separation and reattachment. The separation angularity is avoided by using an inverse technique in which the displacement thickness is prescribed and the pressure is deduced from the resulting solution. The turbulent results appear qualitatively correct despite the use of a two-layer eddy-viscosity model which is generally assumed appropriate only for mild-pressure-gradient flows. A new viscous-inviscid interaction technique is presented in which the inviscid flow is solved inversely by prescribing the pressure from the boundary-layer solution and deducing the new displacement thickness from the solution of a Cauchy integral. Calculations are presented using this interaction procedure for a laminar flow in which separation and reattachment occur on a solid surface.
Document ID
19760002925
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carter, J. E.
(NASA Langley Research Center Hampton, VA, United States)
Wornom, S. F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Aerodynamic Analyses Requiring Advanced Computers, Pt. 1
Subject Category
Aerodynamics
Accession Number
76N10013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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