@inproceedings{d239fb89f3b14c3289d29ac7f80cebb2,
title = "OVERFLOW analysis of the DLR-F11 configuration from HiLiftPW-2 including transition modeling",
abstract = "The OVERFLOW Reynolds-averaged Navier-Stokes solver has been used to predicted the aerodynamic characteristics of the DLR-F11 high-lift configuration for the conditions prescribed in the second AIAA computational fluid dynamics High-Lift Prediction Workshop. A grid convergence study is performed for the geometry with the slat and flap brackets excluded. The influence of including the brackets in the computational geometry is considered, and the effects of varying Reynolds number are analyzed for the brackets-on configuration. An optional case of the workshop, but a focus of this paper, is the inclusion of laminar-turbulent transition in the solutions. Two CFD-compatible transition models are used for the analysis, and their behaviors are discussed. A turbulence model verification study, which was an optional case for the workshop, is also included.",
author = "Coder, \{James G.\}",
year = "2014",
doi = "10.2514/6.2014-2696",
language = "English (US)",
isbn = "9781624102882",
series = "32nd AIAA Applied Aerodynamics Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "32nd AIAA Applied Aerodynamics Conference",
note = "32nd AIAA Applied Aerodynamics Conference 2014 ; Conference date: 16-06-2014 Through 20-06-2014",
}