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Improved numerical methods for turbulent viscous recirculating flowsThe hybrid-upwind finite difference schemes employed in generally available combustor codes possess excessive numerical diffusion errors which preclude accurate quantative calculations. The present study has as its primary objective the identification and assessment of an improved solution algorithm as well as discretization schemes applicable to analysis of turbulent viscous recirculating flows. The assessment is carried out primarily in two dimensional/axisymetric geometries with a view to identifying an appropriate technique to be incorporated in a three-dimensional code.
Document ID
19880001766
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Turan, A.
(Avco-Everett Research Lab. MA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Publication Information
Publication: NASA. Lewis Research Center, Turbine Engine Hot Section Technology, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
88N11148
Funding Number(s)
CONTRACT_GRANT: NAS3-24351
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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