@inproceedings{4de6cda7c83948138a0b639444ac24ca,
title = "ANALYSIS OF A WING-TIP-MOUNTED SMALL-SCALE PROPELLER CONFIGURATION UNDER NON-AXIAL INFLOW CONDITIONS",
abstract = "Regarding the design of the propeller propulsion system of small and medium-sized aircraft and UAVs there is still a need for an aerodynamic analysis of the specific flow characteristics of such vehicles, namely, the combination of small propeller dimensions and a wide range of inflow angles. In this work, a wing-tip-mounted propeller is analyzed both experimentally as well as by URANS calculations. Analyzed are the behavior of time-averaged aerodynamic reaction forces regarding thrust, lift, and pitching moment, the surface pressure along the wing contour, and the occurring flow field.",
keywords = "Drone, Propeller, UAV, URANS, Wind tunnel",
author = "M. Cerny and N. Herzog and C. Breitsamter",
note = "Publisher Copyright: {\textcopyright} 2021 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021. All rights reserved.; 32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021 ; Conference date: 06-09-2021 Through 10-09-2021",
year = "2021",
language = "English",
series = "32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021",
publisher = "International Council of the Aeronautical Sciences",
booktitle = "32nd Congress of the International Council of the Aeronautical Sciences, ICAS 2021",
}