NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Three-dimensional application of the Johnson-King turbulence model for a boundary-layer direct methodThe Johnson-King turbulence model as extended to three-dimensional flows was evaluated using finite-difference boundary-layer direct method. Calculations were compared against the experimental data of the well-known Berg-Elsenaar incompressible flow over an infinite swept-wing. The Johnson-King model, which includes the nonequilibrium effects in a developing turbulent boundary-layer, was found to significantly improve the predictive quality of a direct boundary-layer method. The improvement was especially visible in the computations with increased three-dimensionality of the mean flow, larger integral parameters, and decreasing eddy-viscosity and shear stress magnitudes in the streamwise direction; all in better agreement with the experiment than simple mixing-length methods.
Document ID
19900038822
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kavsaoglu, Mehmet S.
(Middle East Technical University Ankara, Turkey)
Kaynak, Unver
(Turkish Aerospace Industries Kavaklidere, Turkey)
Van Dalsem, William R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: ISCFD Nagoya 1989
Location: Nagoya
Country: Japan
Start Date: August 28, 1989
End Date: August 31, 1989
Sponsors: Gas Turbine Society of Japan, Japan Society of Computational Fluid Dynamics, Architectural Institute of Japan
Accession Number
90A25877
Distribution Limits
Public
Copyright
Other

Available Downloads

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