Roll Control of Morphing Aircraft with Synthetic Jet Actuators at a High Angle of Attack
Flow separation and dynamic stall occurring at a high angle of attack will lead to difficulty in control and maneuverability for morphing aircraft. This study proposes a novel active flow control technology using a synthetic jet actuator for the roll motion of morphing aircraft. With the help of the...
Na minha lista:
| Principais autores: | , , , , |
|---|---|
| Format: | Artigo |
| Sprog: | Inglês |
| Udgivet: |
MDPI AG
2021-01-01
|
| Serier: | Applied Sciences |
| Fag: | |
| Online adgang: | https://www.mdpi.com/2076-3417/11/2/505 |
| Tags: |
Ingen Tags, Vær først til at tagge denne postø!
|