@inproceedings{ac218f2fc8d54a7fac2fd9c1173d8ab6,
title = "Numerical analysis of propeller-wing interaction in aircraft with distributed electric propulsion",
abstract = "The previously-proposed phenomenon of active wingtip vortex cancellation is generalized to aircraft with distributed electric propulsion. Lift and drag are calculated using a sliding mesh CFD model that leverages prior literature for validation. In agreement with previous results, a lift increase of approximately 22\% is found. Unlike previous results, a drag increase of approximately 4\% is found.",
author = "Peter Sharpe and Agarwal, \{Ramesh K.\}",
note = "Publisher Copyright: {\textcopyright} 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Aviation 2019 Forum ; Conference date: 17-06-2019 Through 21-06-2019",
year = "2019",
doi = "10.2514/6.2019-3691",
language = "English",
isbn = "9781624105890",
series = "AIAA Aviation 2019 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
pages = "1--14",
booktitle = "AIAA Aviation 2019 Forum",
}