NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Streamline curvature effects on turbulent boundary layersA theoretical tool has been developed for predicting, in a nonempirical manner, effects of streamline curvature and coordinate-system rotation on turbulent boundary layers. The second-order closure scheme developed by Wilcox and Traci has been generalized for curved streamline flow and for flow in a rotating coordinate system. A physically based straightforward argument shows that curvature/rotation primarily affects the turbulent mixing energy; the argument yields suitable curvature/rotation terms which are added to the mixing-energy equation. Singular-perturbation solutions valid in the wall layer of a curved-wall boundary layer and a fully developed rotating channel flow demonstrate that, with the curvature/rotation terms, the model predicts the curved-wall and the rotating coordinate system laws of the wall. Results of numerical computations of curved-wall boundary layers and of rotating channel flow show that curvature/rotation effects can be computed accurately with second-order closure.
Document ID
19760054039
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wilcox, D. C.
(DCW Industries, Inc. Sherman Oaks, CA, United States)
Chambers, T. L.
(DCW Industries Sherman Oaks, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 76-353
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: San Diego, CA
Start Date: July 14, 1976
End Date: July 16, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A37005
Funding Number(s)
CONTRACT_GRANT: NAS2-9135
CONTRACT_GRANT: NAS2-8884
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available