Issue |
E3S Web Conf.
Volume 459, 2023
XXXIX Siberian Thermophysical Seminar (STS-39)
|
|
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Article Number | 03005 | |
Number of page(s) | 5 | |
Section | Methods for Controlling Turbulence and Intensifying Heat and Mass Transfer | |
DOI | https://doi.org/10.1051/e3sconf/202345903005 | |
Published online | 04 December 2023 |
Features of the flow around the model of a small-sized aircraft of a classical layout with a distributed electric propulsion
Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences, 4/1 Institutskaya Street, Novosibirsk, 630090, Russia
* Corresponding author: melnik1999e@mail.ru
The article presents the results of experimental studies on the influence of the work of a distributed electric propulsion on the flow around the straight wing of a small-sized aircraft. The flow structure was studied at natural (flight) Reynolds numbers, taking into account the angle of attack. The results of the experiments are visualization patterns obtained using the soot-oil coating method.
© The Authors, published by EDP Sciences, 2023
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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