Aero-Propulsive Interactions between UAV Wing and Distributed Propellers Due to Their Relative Position
The purpose of this paper is the evaluation of the aero-propulsive effects on a UAV wing model with distributed propulsion. An array of three propellers is placed ahead of the leading edge of a rectangular wing with flap. The investigation was performed with high-fidelity numerical analyses to provi...
| Автори: | , , , |
|---|---|
| Формат: | Стаття |
| Мова: | English |
| Опубліковано: |
MDPI AG
2023-01-01
|
| Серія: | Drones |
| Предмети: | |
| Онлайн доступ: | https://www.mdpi.com/2504-446X/7/1/49 |