This chapter presents high-order DG solutions of the RANS and k-ω turbulence model equations for transonic flows around aeronautical configurations. A directional shock-capturing term, proportional to the inviscid residual, is employed to control oscillations around shocks. Implicit time integration is applied to the fully coupled RANS and k-ω equations. Several high-order DG results of 2D and 3D transonic turbulent test cases proposed within the ADIGMA project demonstrate the capability of the method. © 2010 Springer-Verlag Berlin Heidelberg.
CITATION STYLE
Bassi, F., Botti, L., Colombo, A., Crivellini, A., Franchina, N., Ghidoni, A., & Rebay, S. (2010). Very high-order accurate discontinuous Galerkin computation of transonic turbulent flows on aeronautical configurations. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 113, 25–38. https://doi.org/10.1007/978-3-642-03707-8_3
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