@inproceedings{21dc90d4cd7248458fb2064426951f1d,
title = "Fast prediction model for tonal noise from rotors",
abstract = "A blade element approach is used to compute the sound from a helicopter rotor in hover. The paper investigates into the effect of the number of chordwise integration panels on the computed aerodynamically generated sound.",
author = "Marinus, {B. G.} and A. Halimi and M. Jeanpierre",
note = "Publisher Copyright: {\textcopyright} 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 22nd AIAA/CEAS Aeroacoustics Conference, 2016 ; Conference date: 30-05-2016 Through 01-06-2016",
year = "2016",
doi = "10.2514/6.2016-2871",
language = "English",
isbn = "9781624103865",
series = "22nd AIAA/CEAS Aeroacoustics Conference, 2016",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "22nd AIAA/CEAS Aeroacoustics Conference",
}