Collaborative Testing of Turbulence Models

Author:

Bradshaw P.1,Launder B. E.2,Lumley J. L.3

Affiliation:

1. Mechanical Engineering Department, Stanford University, Stanford, CA 94305

2. Mechanical Engineering Department, University of Manchester Institute of Science and Technology, Manchester, England

3. Sibley School of Mechanical and Aerospace Engineering, Cornell University, Ithaca, NY

Abstract

This is a brief report on a special project. Data from experiments and simulations were collected and distributed to over 100 turbulence modelers and other participants in 16 different countries. The modelers mailed the results of their “predictions” back to the organizers for distribution to all the participants for comment. The data covered most types of turbulent flow, compressible and incompressible, but the emphasis was on complex (strongly nonequilibrium) flows. No model was capable of predicting the full range of flows to good engineering accuracy, but stress-transport models seemed to perform best. The exchange of views and results alone has been of real benefit to modelers.

Publisher

ASME International

Subject

Mechanical Engineering

Reference6 articles.

1. Baz, A. El, Craft, T. J., Ince, N. Z., and Launder, B. E., 1992, “On the Adequacy of the Thin-Shear-Flow Equations for Computing Turbulent Jets in Stagnant Surroundings,” Manchester University, England, UMIST Rept. TFD/92/1.

2. Coles, D., and Hirst, E. A., (eds.), 1969, Computation of Turbulent Boundary Layers, Vol. 2, Thermosciences Division, Mech Engg Dept, Stanford.

3. Jovic, S., and Driver, D. M., 1993, “Reynolds-Number Effect on Skin Friction in Separated Flows Behind a Backward-Facing Step,” paper in draft.

4. Kline, S. J., Cantwell, B. J., and Lilley, G. M. (Eds.) 1982, Complex Turbulent Shear Flows: Comparison of Computation and Experiment, Thermosciences Division, Mech Engg Dept, Stanford University.

5. Settles, G. S., and Dodson, L., 1993, “Hypersonic Turbulent Boundary-Layer and Free Shear Database,” NASA Contractor Report 177610.

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