Summary
Appropriate three-dimensional equations have been solved, in finite-difference form, and with boundary conditions corresponding to the infinite swept wing of van den Berg and Elsenaar and the full three-dimensional data of East and Hoxey. In the former case, results were obtained with an algebraic eddy-viscosity formulation and a two-equation model which allows for transport of turbulence kinetic energy and dissipation rate. The results show that both models yield similar mean-flow characteristics, provided the same wall boundary conditions are employed, and that these deviate from the measurements with increasing adverse pressure gradient. As with previous investigations of two-dimensional flows, the procedure used to generate the initial turbulence energy profile can significantly influence the calculated results. The calculations of the fully three-dimensional flow made use of the algebraic eddy-viscosity formulation and, in keeping with the previous results for two-dimensional flows and the swept wing, the agreement with measurements is excellent until the separation region is approached.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Cebeci, T. and Meier, H.U.: Modeling Requirements for the Calculation of the Turbulent Flow Around Airfoils, Wings and Bodies of Revolution. AGARD Conference on Turbulent Boundary Layers; Experiments, Theory and Modeling, Den Haag, the Netherlands, 26–26, 1979.
Coles, D. and Hirst, E.A.: Computation of Turbulent Boundary Layers — 1968, AFOSR-IFD-Stanford Conference, Vol. 2, Thermoscience Division, Stanford University, Stanford, 1969.
Cebeci, T. and Smith, A.M.O.: Analysis of Turbulent Boundary Layers, Academic Press, New York, 1974.
Hanjalic, K. and Launder, B.E.: Sensitizing the Dissipation Equation to Irrotational Strains. J. Fluid Engineering, Trans. ASME, Vol. 102, Mar. 1980.
Cebeci, T. and Huang, T.T.: Description of Two Turbulence Models Used in the Finite-Difference Calculation of Three-Dimensional Boundary Layers. Proceedings of Berlin Workshop on Three-Dimensional Boundary Layers, Apr. 1982.
Keller, H.B.: A New Difference Scheme for Parabolic Problems. In Numerical Solution of Partial-Differential Equations. Bramble, J. (ed.), Vol. II, Academic Press, New York, 1970.
Bradshaw, P., Cebeci, T. and Whitelaw, J.H.: Engineering Calculation Methods for Turbulent Flows, Academic Press, London, 1981.
Van den Berg, B., and Elsenaar, A.: Measurements in a Three-Dimensional Incompressible Turbulent Boundary Layer in an Adverse Pressure Gradient Under Infinite Swept-Wing Conditions. NLR TR 72092U, 1972.
East, L.F. and Hoxey, R.P.: Low-Speed Three-Dimensional Turbulent Boundary-Layer Data, Pt. l, Royal Aircraft Establishment, Farnborough, England, TR 69041, Mar. 1969.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1982 Springer-Verlag Berlin Heidelberg
About this chapter
Cite this chapter
Cebeci, T., Chang, K.C. (1982). On the Turbulence-Modeling Requirements of Three-Dimensional Boundary-Layer Flows. In: Haase, W. (eds) Recent Contributions to Fluid Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-81932-2_4
Download citation
DOI: https://doi.org/10.1007/978-3-642-81932-2_4
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-81934-6
Online ISBN: 978-3-642-81932-2
eBook Packages: Springer Book Archive