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Computation of turbulent boundary layers on curved surfaces, 1 June 1975 - 31 January 1976An accurate method was developed for predicting effects of streamline curvature and coordinate system rotation on turbulent boundary layers. A new two-equation model of turbulence was developed which serves as the basis of the study. In developing the new model, physical reasoning is combined with singular perturbation methods to develop a rational, physically-based set of equations which are, on the one hand, as accurate as mixing-length theory for equilibrium boundary layers and, on the other hand, suitable for computing effects of curvature and rotation. The equations are solved numerically for several boundary layer flows over plane and curved surfaces. For incompressible boundary layers, results of the computations are generally within 10% of corresponding experimental data. Somewhat larger discrepancies are noted for compressible applications.
Document ID
19760015067
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wilcox, D. C.
(DCW Industries, Inc. Sherman Oaks, CA, United States)
Chambers, T. L.
(DCW Industries, Inc. Sherman Oaks, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-137853
DCW-R-07-01
Report Number: NASA-CR-137853
Report Number: DCW-R-07-01
Accession Number
76N22155
Funding Number(s)
CONTRACT_GRANT: NAS2-8884
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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