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A high order accurate numerical solution algorithm for turbulent boundary layer flowA fourth-order accurate numerical solution algorithm is derived using finite element interpolation theory for the non-linear parabolic equations governing turbulent boundary layer flow including a two-equation turbulence closure model. The results of carefully controlled numerical experiments firmly quantize for the first time performance differences between finite element and finite difference solution methodology for this type of equation. The developed algorithm takes advantage of the apparent semi-analytical formulational procedure, in establishment of a single, retarded-evaluation Jacobian matrix iterative solution algorithm. Numerical results document performance of solution economy features in terms of computer requirements and solution accuracy. The developed algorithm should find wide application in aerodynamics analysis.
Document ID
19790035457
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Soliman, M. O.
(Tennessee Univ. Knoxville, TN, United States)
Baker, A. J.
(Tennessee, University Knoxville, Tenn., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 79-0001
Report Number: AIAA PAPER 79-0001
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: New Orleans, LA
Start Date: January 15, 1979
End Date: January 17, 1979
Sponsors: American Institute of Aeronautics, Astronautics
Accession Number
79A19470
Funding Number(s)
CONTRACT_GRANT: NSG-1391
Distribution Limits
Public
Copyright
Other

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