@inproceedings{a7ede51789cc425b9e57d4f30c5aab3d,
title = "Investigation of flow phenomena on generic delta wing",
abstract = "A comprehensive experimental research program on a generic delta wing configuration is conducted as part of the {"}International Vortex Flow Experiment 2{"} (VFE-2). The aim of the present study is to set up a validated data base for test of modern CFD codes focusing on methods such as URANS (Unsteady Reynolds Averaged Navier- Stokes) and DES (Detached Eddy Simulation). Flow types of partly developed (α = 13°), fully developed (α = 18°) and burst leading-edge vortices (α = 23° and α = 28°) are investigated for vortices shed at both sharp and rounded leading edges.",
keywords = "Aerodynamics, Experiments, High Angle of Attack, Vortex Flow, Wind Tunnel",
author = "Andrej Furman and Christian Breitsamter",
year = "2006",
language = "English",
isbn = "9781604232271",
series = "ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006",
publisher = "International Council of The Aeronautical Sciences (ICAS)",
pages = "978--993",
booktitle = "ICAS-Secretariat - 25th Congress of the International Council of the Aeronautical Sciences 2006",
note = "25th Congress of the International Council of the Aeronautical Sciences 2006 ; Conference date: 03-09-2006 Through 08-09-2006",
}