NACA 2412 Drag Reduction Using V-Shaped Riblets
This research focuses on addressing a significant concern in the aviation industry, which is drag. The primary objective of this project is to achieve drag reduction through the implementation of riblets on a wing featuring the NACA 2412 aerofoil, operating at subsonic speeds. Riblets, with the flow...
| Váldodahkkit: | , , , |
|---|---|
| Materiálatiipa: | Artihkal |
| Giella: | English |
| Almmustuhtton: |
MDPI AG
2024-05-01
|
| Ráidu: | Eng |
| Fáttát: | |
| Liŋkkat: | https://www.mdpi.com/2673-4117/5/2/51 |