@inproceedings{9e3f3cb153504d668a279bafa31bf0ce,
title = "Numerical study of the aerodynamics of rectangular multi-element wing in ground effect",
abstract = "This paper focuses on simulation of flow past a rectangular multi-element wing with 30P30N airfoil cross-section in ground effect. For validation of the simulation approach, computations are performed for the two-dimensional 30P30N airfoil in unbounded flow and are compared with the experimental data. The commercial CFD solver ANSYS FLUENT is employed in computations. Compressible Reynolds-Averaged Navier-Stokes (RANS) equations in conjunction with Spalart-Allmaras (SA) turbulence model are solved using a finite-volume method. The validated code is employed to simulate the flow field of a rectangular wing with 30P30N three-element airfoil in ground effect. 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} 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 36th AIAA Applied Aerodynamics Conference, 2018 ; Conference date: 25-06-2018 Through 29-06-2018",
year = "2018",
doi = "10.2514/6.2018-4115",
language = "English",
isbn = "9781624105593",
series = "2018 Applied Aerodynamics Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "2018 Applied Aerodynamics Conference",
}