@inproceedings{dc39592dd54d4b83a069367be82eca42,
title = "Numerical study of fuselage aerodynamics of DLR-F6 wing-body in ground effect",
abstract = "The main focus of this paper is on the simulation of flow past a three-dimensional wing-body configuration (DLR-F6) in ground effect. For the purpose of validation of the simulation approach, computations are performed for the DLR-F6 wing-body in unbounded flow and are compared with the experimental data. The commercial CFD solver ANSYS FLUENT is employed for computations. Compressible Reynolds-Averaged Navier-Stokes (RANS) equations in conjunction with Spalart-Allmaras (SA) and K-ω Shear Stress Transport (SST) turbulence models are solved. The validated code is employed to calculate the flow field in ground effect. In particular, the aerodynamics of the fuselage is analyzed in detail. The effects of flight heights above the ground on the aerodynamic properties and flow field are analyzed.",
author = "Ning Deng and Qiulin Qu and Agarwal, {Ramesh K.}",
note = "Publisher Copyright: {\textcopyright} 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 35th AIAA Applied Aerodynamics Conference, 2017 ; Conference date: 05-06-2017 Through 09-06-2017",
year = "2017",
doi = "10.2514/6.2017-4234",
language = "English",
isbn = "9781624105012",
series = "35th AIAA Applied Aerodynamics Conference, 2017",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "35th AIAA Applied Aerodynamics Conference, 2017",
}