@inproceedings{ae1b5a5ef05146c292e04084ad846675,
title = "3D flow features in the boundary layer of a rotating propeller blade",
abstract = "We use lattice Boltzmann unsteady simulations to investigate the pressure and skin friction distribution around propeller blades featuring serrations either at the leading edge or at the trailing edge. Then we look at their overall performance and the vorticity in the neighborhood of serrations. Next to a baseline blade, six serrated geometries with different serrations amplitude and wavelength are analyzed.",
author = "Marinus, \{B. G.\} and C. Irimia and A. Halimi and A. Pire",
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 = "10.2514/6.2019-3293",
language = "English",
isbn = "9781624105890",
series = "AIAA Aviation 2019 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
pages = "1--11",
booktitle = "AIAA Aviation 2019 Forum",
}