@inproceedings{ea58ffd70d78425881ab96ce07bdb060,
title = "Computation of flow field of an airfoil with Gurney flap in ground effect",
abstract = "This paper describes the ground effect aerodynamics of an airfoil with Gurney flap. For this purpose, NACA0012 airfoil with different shapes of Gurney flaps is considered. Computational results from ANSYS FLUENT are compared to the wind tunnel test results to verify the simulation model. Computations are then performed to include the ground effect. Computations show that the presence of the ground mainly affects the size of vortices at the trailing edge of the airfoil resulting in larger lift force and smaller drag force compared to the airfoil in unbounded flow.",
author = "Xuan Zhang 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 = "10.2514/6.2017-4466",
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",
}