Summary
Different turbulence models are applied to the incompressible boundary layer along a flat plate, with a zero, favourable or adverse pressure gradient (test case TC3). The algebraic model of Cebeci & Smith and the k — ω models give the best overall performance.
This is a preview of subscription content, log in via an institution to check access.
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
Lien, F.S. & Leschziner, M.A. 1993 Modelling 2D and 3D separation from curved surfaces with variants of second-moment closure combined with low-Re near-wall formulations. Proc. 9th Symp. on Turbulent Shear Flows, paper 13-1.
Wilcox, D.C. 1993 Turbulence modeling of CFD. DCW Industries Inc.
Hanjalić, K., Jakirlić, Stošić, N., Vasić, S. & Hadžić, I. 1992 Collaborative testing of turbulence models 1990/1992. Report LSTM 352/T/92, Universität Erlangen-Nürnberg.
Nagano, Y., Tagawa, M. & Tsuji, T. 1991 Effects of adverse pressure gradients on mean flows and turbulence statistics in a boundary layer. Proc. 8th Symp. on Turbulent Shear Flows, paper 2–3.
Author information
Authors and Affiliations
Editor information
Rights and permissions
Copyright information
© 1998 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden
About this chapter
Cite this chapter
Henkes, R.A.W.M. (1998). Application of Turbulence Models to Incompressible Boundary Layers in Aeronautics. In: Dervieux, A., Braza, M., Dussauge, JP. (eds) Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA. Notes on Numerical Fluid Mechanics (NNFM), vol 5. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-322-89859-3_22
Download citation
DOI: https://doi.org/10.1007/978-3-322-89859-3_22
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-322-89861-6
Online ISBN: 978-3-322-89859-3
eBook Packages: Springer Book Archive