@inproceedings{e59c885be2d44fb8837ef39b5e04e597,
title = "Implicit Large-Eddy Simulation for swept wing flow using high-resolution methods",
abstract = "A numerical investigation of a fully three-dimensional swept wing geometry featuring separation from a curved leading edge is presented. The Implicit Large-Eddy Simulation strategy based on a third-order high-resolution method for discretising the advective fluxes and a third-order Runge-Kutta time-stepping scheme with extended stability region has been employed. No attempt to incorporate a wall-model has been made. Instead, the boundary layer is fully resolved over the majority of the wing. Qualitative and quantitative comparisons with experimental oil-film visualisations and three-dimensional LDA measurements show very good agreement between the experiment and the numerically predicted flow structures, as well as velocity and stress profiles near the wing. Furthermore, data from a hybrid RANS/LES simulation has been included for comparison.",
author = "M. Hahn and D. Drikakis",
note = "Copyright: Copyright 2020 Elsevier B.V., All rights reserved.",
year = "2008",
doi = "10.2514/6.2008-669",
language = "English",
isbn = "9781563479373",
series = "46th AIAA Aerospace Sciences Meeting and Exhibit",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "46th AIAA Aerospace Sciences Meeting and Exhibit",
}