An experimental and computational investigation of the transport of Reynolds stress in an axisymmetric swirling boundary layer
Abstract
A coordinated experimental and computational investigation of the transport and interaction of the individual Reynolds stresses within a turbulent axisymmetric swirling boundary layer flowing over a stationary cylinder is described. The cylinder is instrumented with new directional surface fence skin-friction gages developed for the experiment. The longitudinal and transverse mean velocity profiles are measured with a miniature directional pressure probe. These data provided a standard on which to compare computed results employing a variety of turbulence models. The turbulence models tested range from a simple mixing length model, through a two-equation model, on to the Reynolds stress equation models. The full Reynolds stress equation models are tested with various sets of modeling coefficients for the pressure rate-of-strain correlation. It is shown that while even the simplest model shows the general features of the data, agreement with the experimental data is enhanced through the use of the more complex models. For a better prediction of the data, however, further model improvement is still required.
- Publication:
-
AIAA, Aerospace Sciences Meeting
- Pub Date:
- January 1981
- Bibcode:
- 1981aiaa.meetS....H
- Keywords:
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- Axisymmetric Flow;
- Computational Fluid Dynamics;
- Reynolds Stress;
- Swirling;
- Turbulent Boundary Layer;
- Velocity Distribution;
- Boundary Layer Equations;
- Computerized Simulation;
- Cylindrical Bodies;
- Skin Friction;
- Turbulence Models;
- Wind Tunnel Tests;
- Fluid Mechanics and Heat Transfer